diff --git a/.agents/AGENTS.md b/.agents/AGENTS.md
new file mode 100644
index 000000000..7073c9b93
--- /dev/null
+++ b/.agents/AGENTS.md
@@ -0,0 +1,82 @@
+# RocketPy Workspace Instructions
+
+## Code Style
+- Use snake_case for variables, functions, methods, and modules. Use descriptive names.
+- Use PascalCase for classes and UPPER_SNAKE_CASE for constants.
+- Keep lines at 88 characters and follow PEP 8 unless existing code in the target file differs.
+- Run Ruff as the source of truth for formatting/import organization:
+  - `make format`
+  - `make lint`
+- Use NumPy-style docstrings for public classes, methods, and functions, including units.
+- In case of tooling drift between docs and config, prefer current repository tooling in `Makefile`
+  and `pyproject.toml`.
+
+## Architecture
+- RocketPy is a modular Python library; keep feature logic in the correct package boundary:
+  - `rocketpy/simulation`: flight simulation and Monte Carlo orchestration.
+  - `rocketpy/rocket`, `rocketpy/motors`, `rocketpy/environment`: domain models.
+  - `rocketpy/mathutils`: numerical primitives and interpolation utilities.
+  - `rocketpy/plots`, `rocketpy/prints`: output and visualization layers.
+- Prefer extending existing classes/patterns over introducing new top-level abstractions.
+- Preserve public API stability in `rocketpy/__init__.py` exports.
+
+## Build and Test
+- Use Makefile targets for OS-agnostic workflows:
+  - `make install`
+  - `make pytest`
+  - `make pytest-slow`
+  - `make coverage`
+  - `make coverage-report`
+  - `make build-docs`
+- Before finishing code changes, run focused tests first, then broader relevant suites.
+- When running Python directly in this workspace, prefer the project virtual
+  environment interpreter: `.venv/bin/python` on Unix/macOS or
+  `.venv/Scripts/python.exe` on Windows.
+- Slow tests are explicitly marked with `@pytest.mark.slow` and are run with `make pytest-slow`.
+- For docs changes, check `make build-docs` output and resolve warnings/errors when practical.
+
+## Development Workflow
+- Target pull requests to `develop` by default; `master` is the stable branch.
+- Use branch names in `type/description` format, such as:
+  - `bug/<description>`
+  - `doc/<description>`
+  - `enh/<description>`
+  - `mnt/<description>`
+  - `tst/<description>`
+- Prefer rebasing feature branches on top of `develop` to keep history linear.
+- Keep commit and PR titles explicit and prefixed with project acronyms when possible:
+  - `BUG`, `DOC`, `ENH`, `MNT`, `TST`, `BLD`, `REL`, `REV`, `STY`, `DEV`.
+
+## Conventions
+- SI units are the default. Document units and coordinate-system references explicitly.
+- Position/reference-frame arguments are critical in this codebase. Be explicit about orientation
+  (for example, `tail_to_nose`, `nozzle_to_combustion_chamber`).
+- Include unit tests for new behavior. Follow AAA structure and clear test names.
+- Use fixtures from `tests/fixtures`; if adding a new fixture module, update `tests/conftest.py`.
+- Use `pytest.approx` for floating-point checks where appropriate.
+- Use `@cached_property` for expensive computations when helpful, and be careful with stale-cache
+  behavior when underlying mutable state changes.
+- Keep behavior backward compatible across the public API exported via `rocketpy/__init__.py`.
+- Prefer extending existing module patterns over creating new top-level package structure.
+
+## Testing Taxonomy
+- Unit tests are mandatory for new behavior.
+- Unit tests in RocketPy can be sociable (real collaborators allowed) but should still be fast and
+  method-focused.
+- Treat tests as integration tests when they are strongly I/O-oriented or broad across many methods,
+  including `all_info()` convention cases.
+- Acceptance tests represent realistic user/flight scenarios and may compare simulation thresholds to
+  known flight data.
+
+## Documentation Links
+- Contributor workflow and setup: `docs/development/setting_up.rst`
+- Style and naming details: `docs/development/style_guide.rst`
+- Testing philosophy and structure: `docs/development/testing.rst`
+- API reference conventions: `docs/reference/index.rst`
+- Domain/physics background: `docs/technical/index.rst`
+
+## Scoped Customizations
+- Simulation-specific rules: `.agents/skills/simulation-safety/SKILL.md`
+- Test-authoring rules: `.agents/skills/tests-python/SKILL.md`
+- RST/Sphinx documentation rules: `.agents/skills/sphinx-docs/SKILL.md`
+- Specialized review persona: `.agents/skills/rocketpy-reviewer/SKILL.md`
diff --git a/.agents/skills/rocketpy-reviewer/SKILL.md b/.agents/skills/rocketpy-reviewer/SKILL.md
new file mode 100644
index 000000000..30d3f7598
--- /dev/null
+++ b/.agents/skills/rocketpy-reviewer/SKILL.md
@@ -0,0 +1,62 @@
+---
+description: "Physics-safe RocketPy code review agent. Use for pull request review, unit consistency checks, coordinate-frame validation, cached-property risk detection, and regression-focused test-gap analysis."
+name: "RocketPy Reviewer"
+tools: [read, search]
+argument-hint: "Review these changes for physics correctness and regression risk: <scope or files>"
+user-invocable: true
+---
+You are a RocketPy-focused reviewer for physics safety and regression risk.
+
+## Goals
+
+- Detect behavioral regressions and numerical/physics risks before merge.
+- Validate unit consistency and coordinate/reference-frame correctness.
+- Identify stale-cache risks when `@cached_property` interacts with mutable state.
+- Check test coverage quality for changed behavior.
+- Verify alignment with RocketPy workflow and contributor conventions.
+
+## Review Priorities
+
+1. Correctness and safety issues (highest severity).
+2. Behavioral regressions and API compatibility.
+3. Numerical stability and tolerance correctness.
+4. Missing tests or weak assertions.
+5. Documentation mismatches affecting users.
+6. Workflow violations (test placement, branch/PR conventions, or missing validation evidence).
+
+## RocketPy-Specific Checks
+
+- SI units are explicit and consistent.
+- Orientation conventions are unambiguous (`tail_to_nose`, `nozzle_to_combustion_chamber`, etc.).
+- New/changed simulation logic does not silently invalidate cached values.
+- Floating-point assertions use `pytest.approx` where needed.
+- New fixtures are wired through `tests/conftest.py` when applicable.
+- Test type is appropriate for scope (`unit`, `integration`, `acceptance`) and `all_info()`-style tests
+  are not misclassified.
+- New behavior includes at least one regression-oriented test and relevant edge-case checks.
+- For docs-affecting changes, references and paths remain valid and build warnings are addressed.
+- Tooling recommendations match current repository setup (prefer Makefile plus `pyproject.toml`
+  settings when docs are outdated).
+
+## Validation Expectations
+
+- Prefer focused test runs first, then broader relevant suites.
+- Recommend `make format` and `make lint` when style/lint risks are present.
+- Recommend `make build-docs` when `.rst` files or API docs are changed.
+
+## Output Format
+
+Provide findings first, ordered by severity.
+For each finding include:
+- Severity: Critical, High, Medium, or Low
+- Location: file path and line
+- Why it matters: behavioral or physics risk
+- Suggested fix: concrete, minimal change
+
+After findings, include:
+- Open questions or assumptions
+- Residual risks or testing gaps
+- Brief change summary
+- Suggested validation commands (only when useful)
+
+If no findings are identified, state that explicitly and still report residual risks/testing gaps.
diff --git a/.agents/skills/simulation-safety/SKILL.md b/.agents/skills/simulation-safety/SKILL.md
new file mode 100644
index 000000000..cc2af5d27
--- /dev/null
+++ b/.agents/skills/simulation-safety/SKILL.md
@@ -0,0 +1,41 @@
+---
+description: "Use when editing rocketpy/simulation code, including Flight state updates, Monte Carlo orchestration, post-processing, or cached computations. Covers simulation state safety, unit/reference-frame clarity, and regression checks."
+name: "Simulation Safety"
+applyTo: "rocketpy/simulation/**/*.py"
+---
+# Simulation Safety Guidelines
+
+- Keep simulation logic inside `rocketpy/simulation` and avoid leaking domain behavior that belongs in
+  `rocketpy/rocket`, `rocketpy/motors`, or `rocketpy/environment`.
+- Preserve public API behavior and exported names used by `rocketpy/__init__.py`.
+- Prefer extending existing simulation components before creating new abstractions:
+  - `flight.py`: simulation state, integration flow, and post-processing.
+  - `monte_carlo.py`: orchestration and statistical execution workflows.
+  - `flight_data_exporter.py` and `flight_data_importer.py`: persistence and interchange.
+  - `flight_comparator.py`: comparative analysis outputs.
+- Be explicit with physical units and reference frames in new parameters, attributes, and docstrings.
+- For position/orientation-sensitive behavior, use explicit conventions (for example
+  `tail_to_nose`, `nozzle_to_combustion_chamber`) and avoid implicit assumptions.
+- Treat state mutation carefully when cached values exist.
+- If changes can invalidate `@cached_property` values, either avoid post-computation mutation or
+  explicitly invalidate affected caches in a controlled, documented way.
+- Keep numerical behavior deterministic unless stochastic behavior is intentional and documented.
+- For Monte Carlo and stochastic code paths, make randomness controllable and reproducible when tests
+  rely on it.
+- Prefer vectorized NumPy operations for hot paths and avoid introducing Python loops in
+  performance-critical sections without justification.
+- Guard against numerical edge cases (zero/near-zero denominators, interpolation limits, and boundary
+  conditions).
+- Do not change default numerical tolerances or integration behavior without documenting motivation and
+  validating regression impact.
+- Add focused regression tests for changed behavior, including edge cases and orientation-dependent
+  behavior.
+- For floating-point expectations, use `pytest.approx` with meaningful tolerances.
+- Run focused tests first, then broader relevant tests (`make pytest` and `make pytest-slow` when
+  applicable).
+
+See:
+- `docs/development/testing.rst`
+- `docs/development/style_guide.rst`
+- `docs/development/setting_up.rst`
+- `docs/technical/index.rst`
diff --git a/.agents/skills/sphinx-docs/SKILL.md b/.agents/skills/sphinx-docs/SKILL.md
new file mode 100644
index 000000000..8c24cac53
--- /dev/null
+++ b/.agents/skills/sphinx-docs/SKILL.md
@@ -0,0 +1,32 @@
+---
+description: "Use when writing or editing docs/**/*.rst. Covers Sphinx/reStructuredText conventions, cross-references, toctree hygiene, and RocketPy unit/reference-frame documentation requirements."
+name: "Sphinx RST Conventions"
+applyTo: "docs/**/*.rst"
+---
+# Sphinx and RST Guidelines
+
+- Follow existing heading hierarchy and style in the target document.
+- Prefer linking to existing documentation pages instead of duplicating content.
+- Use Sphinx cross-references where appropriate (`:class:`, `:func:`, `:mod:`, `:doc:`, `:ref:`).
+- Keep API names and module paths consistent with current code exports.
+- Document physical units and coordinate/reference-frame conventions explicitly.
+- Include concise, practical examples when introducing new user-facing behavior.
+- Keep prose clear and technical; avoid marketing language in development/reference docs.
+- When adding a new page, update the relevant `toctree` so it appears in navigation.
+- Use RocketPy docs build workflow:
+  - `make build-docs` from repository root for normal validation.
+  - If stale artifacts appear, clean docs build outputs via `cd docs && make clean`, then rebuild.
+- Treat new Sphinx warnings/errors as issues to fix or explicitly call out in review notes.
+- Keep `docs/index.rst` section structure coherent with user, development, reference, technical, and
+  examples navigation.
+- Do not edit Sphinx-generated scaffolding files unless explicitly requested:
+  - `docs/Makefile`
+  - `docs/make.bat`
+- For API docs, ensure references remain aligned with exported/public objects and current module paths.
+
+See:
+- `docs/index.rst`
+- `docs/development/build_docs.rst`
+- `docs/development/style_guide.rst`
+- `docs/reference/index.rst`
+- `docs/technical/index.rst`
diff --git a/.agents/skills/tests-python/SKILL.md b/.agents/skills/tests-python/SKILL.md
new file mode 100644
index 000000000..1e9626142
--- /dev/null
+++ b/.agents/skills/tests-python/SKILL.md
@@ -0,0 +1,36 @@
+---
+description: "Use when creating or editing pytest files in tests/. Enforces AAA structure, naming conventions, fixture usage, parameterization, slow-test marking, and numerical assertion practices for RocketPy."
+name: "RocketPy Pytest Standards"
+applyTo: "tests/**/*.py"
+---
+# RocketPy Test Authoring Guidelines
+
+- Unit tests are mandatory for new behavior.
+- Follow AAA structure in each test: Arrange, Act, Assert.
+- Use descriptive test names matching project convention:
+  - `test_methodname`
+  - `test_methodname_stateundertest`
+  - `test_methodname_expectedbehaviour`
+- Include docstrings that clearly state expected behavior and context.
+- Prefer parameterization for scenario matrices instead of duplicated tests.
+- Classify tests correctly:
+  - `tests/unit`: fast, method-focused tests (sociable unit tests are acceptable in RocketPy).
+  - `tests/integration`: broad multi-method/component interactions and strongly I/O-oriented cases.
+  - `tests/acceptance`: realistic end-user/flight scenarios with threshold-based expectations.
+- By RocketPy convention, tests centered on `all_info()` behavior are integration tests.
+- Reuse fixtures from `tests/fixtures` whenever possible.
+- Keep fixture organization aligned with existing categories under `tests/fixtures`
+  (environment, flight, motor, rockets, surfaces, units, etc.).
+- If you add a new fixture module, update `tests/conftest.py` so fixtures are discoverable.
+- Keep tests deterministic: set seeds when randomness is involved and avoid unstable external
+  dependencies unless integration behavior explicitly requires them.
+- Use `pytest.approx` for floating-point comparisons with realistic tolerances.
+- Mark expensive tests with `@pytest.mark.slow` and ensure they can run under the project slow-test
+  workflow.
+- Include at least one negative or edge-case assertion for new behaviors.
+- When adding a bug fix, include a regression test that fails before the fix and passes after it.
+
+See:
+- `docs/development/testing.rst`
+- `docs/development/style_guide.rst`
+- `docs/development/setting_up.rst`
diff --git a/.claude/hooks/README.md b/.claude/hooks/README.md
new file mode 100644
index 000000000..9ddfe1a89
--- /dev/null
+++ b/.claude/hooks/README.md
@@ -0,0 +1,40 @@
+# Claude Code hooks
+
+Project-level [Claude Code hooks](https://docs.claude.com/en/docs/claude-code/hooks)
+that keep Claude's edits lint-clean and stop lint failures from reaching CI. They
+are wired up in [`.claude/settings.json`](../settings.json) and run automatically
+for anyone using Claude Code in this repo.
+
+Both hooks only run **ruff** (the fast linter/formatter, ~0.15s for the whole
+repo). Pylint is intentionally left to CI: on this codebase its per-file startup
+cost is seconds, too slow for an interactive guard. ruff is also what has actually
+been breaking the `Linters` job.
+
+## Hooks
+
+| Hook | Event | What it does |
+| --- | --- | --- |
+| [`ruff_on_edit.py`](ruff_on_edit.py) | `PostToolUse` on `Edit`/`Write`/`MultiEdit` | After Claude edits a `.py` file, runs `ruff format` then `ruff check --fix` on that one file. Surfaces any unfixable lint issues back to Claude. |
+| [`ruff_guard_push.py`](ruff_guard_push.py) | `PreToolUse` on `Bash` | Before a `git push`, runs `ruff check` + `ruff format --check` over the repo and **blocks the push** if either would fail (i.e. before it turns CI red). |
+
+## Design guarantees
+
+- **Cross-platform** (Windows / macOS / Linux): pure Python, no shell built-ins,
+  no OS-specific paths. ruff is invoked as `<current python> -m ruff` so it
+  resolves to the same environment the hook runs in.
+- **Never gets in the way**: if `ruff` is not installed, both hooks are a silent
+  no-op. The push guard only acts on actual `git push` commands.
+
+## Requirements
+
+A working `python` on `PATH` (an activated virtualenv is the normal setup) with
+`ruff` installed: `pip install ruff` — already included in `pip install .[tests]`.
+
+## Testing a hook manually
+
+Pipe a sample event payload to a hook on stdin:
+
+```bash
+printf '{"tool_input":{"file_path":"some_file.py"}}' | python .claude/hooks/ruff_on_edit.py
+printf '{"tool_input":{"command":"git push"}}'      | python .claude/hooks/ruff_guard_push.py
+```
diff --git a/.claude/hooks/ruff_guard_push.py b/.claude/hooks/ruff_guard_push.py
new file mode 100644
index 000000000..651e96a43
--- /dev/null
+++ b/.claude/hooks/ruff_guard_push.py
@@ -0,0 +1,78 @@
+#!/usr/bin/env python3
+"""Claude Code ``PreToolUse`` hook: block ``git push`` if ruff would fail in CI.
+
+Runs before every ``Bash`` command. If the command is a ``git push``, it runs the
+two fast ruff steps from the Linters CI job (``ruff check .`` and
+``ruff format --check .``) over the repo. If either would fail, the push is
+blocked (exit code 2) and the failure is reported back to Claude so it gets fixed
+*before* it turns the CI red.
+
+Only ruff runs here (both steps together are ~0.15s). Pylint is intentionally left
+to CI: on this repo pylint costs seconds-per-file of startup, which is too slow for
+an interactive guard. ruff is what has actually been breaking the Linters job.
+
+Design notes
+------------
+* ruff is invoked as ``<current python> -m ruff`` (see ``ruff_on_edit.py``).
+* Cross-platform: pure Python, no shell built-ins, no OS-specific paths.
+* Silent no-op when the command is not a push, or when ruff is not installed.
+"""
+
+import importlib.util
+import json
+import os
+import re
+import subprocess
+import sys
+
+# Match ``git push`` as a real command (start of line or after a shell
+# separator), tolerating global flags like ``git -C . push``. Avoids most
+# false positives from the substring "push" appearing elsewhere.
+_GIT_PUSH = re.compile(r"(?:^|[\s;&|(`])git(?:\s+-\S+|\s+--\S+)*\s+push\b")
+
+
+def main() -> int:
+    try:
+        payload = json.load(sys.stdin)
+    except (json.JSONDecodeError, ValueError):
+        return 0
+
+    command = (payload.get("tool_input") or {}).get("command", "")
+    if not isinstance(command, str) or not _GIT_PUSH.search(command):
+        return 0
+
+    if importlib.util.find_spec("ruff") is None:
+        return 0  # ruff not installed: don't block pushes.
+
+    # Target the project root explicitly. ``CLAUDE_PROJECT_DIR`` is set by Claude
+    # Code to the native-format project root; passing it as a path argument (not
+    # as the subprocess ``cwd``) keeps this robust across platforms/shells. Falls
+    # back to ".", which resolves against the hook's working directory.
+    target = os.environ.get("CLAUDE_PROJECT_DIR") or "."
+    ruff = [sys.executable, "-m", "ruff"]
+    check = subprocess.run(ruff + ["check", target], capture_output=True, text=True)
+    fmt = subprocess.run(
+        ruff + ["format", "--check", target], capture_output=True, text=True
+    )
+    if check.returncode == 0 and fmt.returncode == 0:
+        return 0
+
+    out = [
+        "[ruff] Push blocked — this would fail the Linters CI job. "
+        "Fix the issues below, then push again.\n"
+    ]
+    if check.returncode != 0:
+        out.append("--- ruff check ---\n" + (check.stdout or "") + (check.stderr or ""))
+    if fmt.returncode != 0:
+        out.append(
+            "--- ruff format --check . ---\n"
+            + (fmt.stdout or "")
+            + (fmt.stderr or "")
+            + "\nFix formatting with:  python -m ruff format .\n"
+        )
+    sys.stderr.write("\n".join(out))
+    return 2
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/.claude/hooks/ruff_on_edit.py b/.claude/hooks/ruff_on_edit.py
new file mode 100644
index 000000000..fa9895119
--- /dev/null
+++ b/.claude/hooks/ruff_on_edit.py
@@ -0,0 +1,60 @@
+#!/usr/bin/env python3
+"""Claude Code ``PostToolUse`` hook: auto-format + lint-fix edited Python files.
+
+Runs after every ``Edit``/``Write``/``MultiEdit``. Reads the hook payload from
+stdin, and if the touched file is a ``.py`` file, runs ``ruff format`` followed by
+``ruff check --fix`` on *just that one file*. ruff is ~instant per file, so this
+keeps Claude's edits continuously formatted and lint-clean without slowing the
+session down.
+
+Design notes
+------------
+* ruff is invoked as ``<current python> -m ruff`` so it always resolves to the
+  same environment the hook runs in (matches the ``python -m ruff`` convention
+  the repo already uses) instead of relying on a ``ruff`` binary being on PATH.
+* Cross-platform: pure Python, no shell built-ins, no OS-specific paths.
+* Degrades to a silent no-op when ruff is not installed, so it can never block
+  editing for a contributor who has not installed the linter yet.
+* Exit code 2 feeds any *unfixable* lint issues back to Claude so it fixes them;
+  the common case (format + autofix succeed) exits 0 silently.
+"""
+
+import importlib.util
+import json
+import subprocess
+import sys
+
+
+def main() -> int:
+    try:
+        payload = json.load(sys.stdin)
+    except (json.JSONDecodeError, ValueError):
+        return 0
+
+    tool_input = payload.get("tool_input") or {}
+    file_path = tool_input.get("file_path")
+    if not isinstance(file_path, str) or not file_path.endswith(".py"):
+        return 0
+
+    if importlib.util.find_spec("ruff") is None:
+        # ruff not installed in this environment: never block the workflow.
+        return 0
+
+    ruff = [sys.executable, "-m", "ruff"]
+    subprocess.run(ruff + ["format", file_path], capture_output=True, text=True)
+    fix = subprocess.run(
+        ruff + ["check", "--fix", file_path], capture_output=True, text=True
+    )
+
+    if fix.returncode != 0:
+        sys.stderr.write(
+            f"[ruff] Lint issues ruff could not auto-fix in {file_path}:\n"
+            f"{fix.stdout}{fix.stderr}"
+        )
+        return 2
+
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/.claude/settings.json b/.claude/settings.json
new file mode 100644
index 000000000..91e8faa2b
--- /dev/null
+++ b/.claude/settings.json
@@ -0,0 +1,46 @@
+{
+  "permissions": {
+    "allow": [
+      "Bash(git fetch *)",
+      "Bash(git merge *)",
+      "Bash(git checkout *)",
+      "Bash(python -m ruff --version)",
+      "Bash(python -m pylint --version)",
+      "Bash(python -m ruff check rocketpy/plots/flight_plots.py tests/unit/test_plots.py)",
+      "Bash(python -m ruff format --check rocketpy/plots/flight_plots.py tests/unit/test_plots.py)",
+      "Bash(python -m ruff check .)",
+      "Bash(python -m ruff format --check .)",
+      "Bash(python -m pylint rocketpy/plots/flight_plots.py tests/unit/test_plots.py)",
+      "Bash(python -m ruff check rocketpy/plots/flight_plots.py)",
+      "Bash(python -m ruff format --check rocketpy/plots/flight_plots.py)",
+      "Bash(python -m pytest tests/unit/test_plots.py -k \"animate_trajectory or animate_rotate\" -p no:cacheprovider -q)",
+      "Bash(python -m pytest tests/unit/test_plots.py -p no:cacheprovider -q)"
+    ]
+  },
+  "hooks": {
+    "PostToolUse": [
+      {
+        "matcher": "Edit|Write|MultiEdit",
+        "hooks": [
+          {
+            "type": "command",
+            "command": "python .claude/hooks/ruff_on_edit.py",
+            "statusMessage": "ruff: formatting edited file"
+          }
+        ]
+      }
+    ],
+    "PreToolUse": [
+      {
+        "matcher": "Bash",
+        "hooks": [
+          {
+            "type": "command",
+            "command": "python .claude/hooks/ruff_guard_push.py",
+            "statusMessage": "ruff: pre-push lint guard"
+          }
+        ]
+      }
+    ]
+  }
+}
diff --git a/.claude/skills/rocketpy-release/SKILL.md b/.claude/skills/rocketpy-release/SKILL.md
new file mode 100644
index 000000000..ebf8acd57
--- /dev/null
+++ b/.claude/skills/rocketpy-release/SKILL.md
@@ -0,0 +1,142 @@
+---
+name: rocketpy-release
+description: >-
+  Cut a new RocketPy release: prepare the version-bump branch, update the
+  changelog and all version references, and guide the PR-to-master + PyPI flow.
+  Use when the user wants to release a new version (e.g. "release v1.13",
+  "fazer um release", "bump version and cut a release", "REL PR").
+---
+
+# RocketPy Release
+
+Prepare and guide a RocketPy version release following the team's established
+`REL:` pattern. This skill prepares the branch and the version-bump commit; the
+human opens the PR and publishes the GitHub Release themselves.
+
+## Branching model
+
+RocketPy uses **`develop`** (integration) and **`master`** (released). All
+feature/fix work lands on `develop`. A release promotes `develop` → `master`.
+
+Since **v1.12.0** the team uses a **single streamlined PR** (see PR #935):
+one `rel/vX.Y.Z` branch — created off `develop`, with the version already
+bumped — opened **straight to `master`**. (Older releases used three PRs; do
+NOT revive that.)
+
+PyPI is published automatically by `.github/workflows/publish-to-pypi.yml` when
+a **GitHub Release is published** (`on: release: [published]`). Creating the
+release/tag in the GitHub UI is the final manual trigger.
+
+## Before you start — gather state
+
+Run these and confirm with the user:
+
+```bash
+git fetch origin
+grep -m1 '^version' pyproject.toml                 # current version
+git show origin/master:pyproject.toml | grep -m1 '^version'   # released version
+git rev-list --left-right --count origin/master...origin/develop  # ahead/behind
+git tag --sort=-creatordate | head -5              # last tags
+```
+
+Confirm the **target version** (semver: MAJOR.MINOR.PATCH) with the user before
+touching files. Never guess the number.
+
+## Step 1 — Create the release branch
+
+Branch off the latest `develop`:
+
+```bash
+git checkout develop && git pull origin develop
+git checkout -b rel/vX.Y.Z
+```
+
+## Step 2 — The version-bump commit
+
+Update **every** version reference. These have been missed before (e.g.
+`installation.rst` sat stale at 1.11.0 through 1.12.x) — check all of them:
+
+| File | What to change |
+|------|----------------|
+| `pyproject.toml` | `version = "X.Y.Z"` |
+| `docs/conf.py` | `release = "X.Y.Z"` and `copyright = "<year>, RocketPy Team"` |
+| `docs/user/installation.rst` | `pip install rocketpy==X.Y.Z` |
+| `CHANGELOG.md` | see below |
+
+Sanity-sweep for any other stragglers (ignore `.venv`):
+
+```bash
+grep -rn "<OLD_VERSION>" --include=*.py --include=*.toml --include=*.rst . \
+  | grep -v '.venv'
+```
+
+### CHANGELOG.md
+
+The changelog `[Unreleased]` section is auto-populated on every merge to
+`develop` by `.github/workflows/changelog.yml`, so entries should already be
+present. To release:
+
+1. Rename the current `## [Unreleased] - yyyy-mm-dd` header to
+   `## [vX.Y.Z] - YYYY-MM-DD` (today's date).
+2. Insert a **fresh empty** `[Unreleased]` block above it, preserving the
+   template comment and empty subsections:
+
+   ```markdown
+   ## [Unreleased] - yyyy-mm-dd
+
+   <!-- These are the changes that were not released yet, please add them correctly.
+   Attention: The newest changes should be on top -->
+
+   ### Added
+
+   ### Changed
+
+   ### Fixed
+   ```
+3. Add a `Changed` entry to the released section for the bump itself:
+   `- REL: bumps up rocketpy version to X.Y.Z [#PR](https://github.com/RocketPy-Team/RocketPy/pull/PR)`
+   (fill the PR number after the PR is opened, or leave a placeholder to edit).
+4. Prune obvious noise if the maintainer wants (tests, CI, merge commits are
+   not meant to be in the changelog per the file's own header comment).
+
+### Commit
+
+Match the historical message style (`REL: bump version to X.Y.Z`):
+
+```bash
+git add pyproject.toml docs/conf.py docs/user/installation.rst CHANGELOG.md
+git commit -m "REL: bumps up rocketpy version to X.Y.Z"
+```
+
+Keep it to **one** bump commit. Do not include unrelated changes.
+
+## Step 3 — Push and hand off the PR
+
+```bash
+git push -u origin rel/vX.Y.Z
+```
+
+**Stop here and let the human open the PR** (team preference — they open it
+themselves). Give them the ready-to-use details:
+
+- **Base:** `master`  ←  **Compare:** `rel/vX.Y.Z`
+- **Title:** `REL: vX.Y.Z` (or `Rel/vX.Y.Z`)
+- **Body:** summarize the highlights; note the single-PR-to-master approach.
+
+## Step 4 — After the PR merges (guide the human)
+
+1. **Sync `master` back into `develop`** so develop carries the new version and
+   the merge history. Historically a PR titled like
+   `MNT: update develop to release vX.Y.Z`, base `develop` ← compare `master`.
+2. **Create the GitHub Release** in the UI: new tag `vX.Y.Z` targeting
+   `master`, title `vX.Y.Z`, paste the changelog section as notes, Publish.
+   → This triggers `publish-to-pypi.yml` and ships to PyPI.
+3. Verify the PyPI publish workflow succeeded and the new version is live.
+
+## Guardrails
+
+- Only prepare the branch + bump commit. **Do not open the PR or publish the
+  release** unless the user explicitly asks — they do those steps themselves.
+- Confirm the target version with the user before editing.
+- Base the PR on **`master`**, not `develop`.
+- One clean `REL:` commit; no unrelated edits.
diff --git a/.github/agents/rocketpy-reviewer.agent.md b/.github/agents/rocketpy-reviewer.agent.md
new file mode 100644
index 000000000..be1b64b13
--- /dev/null
+++ b/.github/agents/rocketpy-reviewer.agent.md
@@ -0,0 +1,62 @@
+---
+description: "Physics-safe RocketPy code review agent. Use for pull request review, unit consistency checks, coordinate-frame validation, cached-property risk detection, and regression-focused test-gap analysis."
+name: "RocketPy Reviewer"
+tools: [read, search, execute]
+argument-hint: "Review these changes for physics correctness and regression risk: <scope or files>"
+user-invocable: true
+---
+You are a RocketPy-focused reviewer for physics safety and regression risk.
+
+## Goals
+
+- Detect behavioral regressions and numerical/physics risks before merge.
+- Validate unit consistency and coordinate/reference-frame correctness.
+- Identify stale-cache risks when `@cached_property` interacts with mutable state.
+- Check test coverage quality for changed behavior.
+- Verify alignment with RocketPy workflow and contributor conventions.
+
+## Review Priorities
+
+1. Correctness and safety issues (highest severity).
+2. Behavioral regressions and API compatibility.
+3. Numerical stability and tolerance correctness.
+4. Missing tests or weak assertions.
+5. Documentation mismatches affecting users.
+6. Workflow violations (test placement, branch/PR conventions, or missing validation evidence).
+
+## RocketPy-Specific Checks
+
+- SI units are explicit and consistent.
+- Orientation conventions are unambiguous (`tail_to_nose`, `nozzle_to_combustion_chamber`, etc.).
+- New/changed simulation logic does not silently invalidate cached values.
+- Floating-point assertions use `pytest.approx` where needed.
+- New fixtures are wired through `tests/conftest.py` when applicable.
+- Test type is appropriate for scope (`unit`, `integration`, `acceptance`) and `all_info()`-style tests
+  are not misclassified.
+- New behavior includes at least one regression-oriented test and relevant edge-case checks.
+- For docs-affecting changes, references and paths remain valid and build warnings are addressed.
+- Tooling recommendations match current repository setup (prefer Makefile plus `pyproject.toml`
+  settings when docs are outdated).
+
+## Validation Expectations
+
+- Prefer focused test runs first, then broader relevant suites.
+- Recommend `make format` and `make lint` when style/lint risks are present.
+- Recommend `make build-docs` when `.rst` files or API docs are changed.
+
+## Output Format
+
+Provide findings first, ordered by severity.
+For each finding include:
+- Severity: Critical, High, Medium, or Low
+- Location: file path and line
+- Why it matters: behavioral or physics risk
+- Suggested fix: concrete, minimal change
+
+After findings, include:
+- Open questions or assumptions
+- Residual risks or testing gaps
+- Brief change summary
+- Suggested validation commands (only when useful)
+
+If no findings are identified, state that explicitly and still report residual risks/testing gaps.
diff --git a/.github/copilot-instructions.md b/.github/copilot-instructions.md
index f5366cb3b..382aa15e0 100644
--- a/.github/copilot-instructions.md
+++ b/.github/copilot-instructions.md
@@ -1,221 +1,80 @@
-# GitHub Copilot Instructions for RocketPy
-
-This file provides instructions for GitHub Copilot when working on the RocketPy codebase.
-These guidelines help ensure consistency with the project's coding standards and development practices.
-
-## Project Overview
-
-RocketPy is a Python library for 6-DOF rocket trajectory simulation.
-It's designed for high-power rocketry applications with focus on accuracy, performance, and ease of use.
-
-## Coding Standards
-
-### Naming Conventions
-- **Use `snake_case` for all new code** - variables, functions, methods, and modules
-- **Use descriptive names** - prefer `angle_of_attack` over `a` or `alpha`
-- **Class names use PascalCase** - e.g., `SolidMotor`, `Environment`, `Flight`
-- **Constants use UPPER_SNAKE_CASE** - e.g., `DEFAULT_GRAVITY`, `EARTH_RADIUS`
-
-### Code Style
-- Follow **PEP 8** guidelines
-- Line length: **88 characters** (Black's default)
-- Organize imports with **isort**
-- Our official formatter is the **ruff frmat**
-
-### Documentation
-- **All public classes, methods, and functions must have docstrings**
-- Use **NumPy style docstrings**
-- Include **Parameters**, **Returns**, and **Examples** sections
-- Document **units** for physical quantities (e.g., "in meters", "in radians")
-
-### Testing
-- Write **unit tests** for all new features using pytest
-- Follow **AAA pattern** (Arrange, Act, Assert)
-- Use descriptive test names following: `test_methodname_expectedbehaviour`
-- Include test docstrings explaining expected behavior
-- Use **parameterization** for testing multiple scenarios
-- Create pytest fixtures to avoid code repetition
-
-## Domain-Specific Guidelines
-
-### Physical Units and Conventions
-- **SI units by default** - meters, kilograms, seconds, radians
-- **Document coordinate systems** clearly (e.g., "tail_to_nose", "nozzle_to_combustion_chamber")
-- **Position parameters** are critical - always document reference points
-- Use **descriptive variable names** for physical quantities
-
-### Rocket Components
-- **Motors**: SolidMotor, HybridMotor and LiquidMotor classes are children classes of the Motor class
-- **Aerodynamic Surfaces**: They have Drag curves and lift coefficients
-- **Parachutes**: Trigger functions, deployment conditions
-- **Environment**: Atmospheric models, weather data, wind profiles
-
-### Mathematical Operations
-- Use **numpy arrays** for vectorized operations (this improves performance)
-- Prefer **scipy functions** for numerical integration and optimization
-- **Handle edge cases** in calculations (division by zero, sqrt of negative numbers)
-- **Validate input ranges** for physical parameters
-- Monte Carlo simulations: sample from `numpy.random` for random number generation and creates several iterations to assess uncertainty in simulations.
-
-## File Structure and Organization
-
-### Source Code Organization
-
-Reminds that `rocketpy` is a Python package served as a library, and its source code is organized into several modules to facilitate maintainability and clarity. The following structure is recommended:
-
-```
-rocketpy/
-├── core/           # Core simulation classes
-├── motors/         # Motor implementations
-├── environment/    # Atmospheric and environmental models
-├── plots/          # Plotting and visualization
-├── tools/          # Utility functions
-└── mathutils/      # Mathematical utilities
-```
-
-Please refer to popular Python packages like `scipy`,  `numpy`, and `matplotlib` for inspiration on module organization.
-
-### Test Organization
-```
-tests/
-├── unit/           # Unit tests
-├── integration/    # Integration tests
-├── acceptance/     # Acceptance tests
-└── fixtures/       # Test fixtures organized by component
-```
-
-### Documentation Structure
-```
-docs/
-├── user/           # User guides and tutorials
-├── development/    # Development documentation
-├── reference/      # API reference
-├── examples/       # Flight examples and notebooks
-└── technical/      # Technical documentation
-```
-
-## Common Patterns and Practices
-
-### Error Handling
-- Use **descriptive error messages** with context
-- **Validate inputs** at class initialization and method entry
-- Raise **appropriate exception types** (ValueError, TypeError, etc.)
-- Include **suggestions for fixes** in error messages
-
-### Performance Considerations
-- Use **vectorized operations** where possible
-- **Cache expensive computations** when appropriate (we frequently use `cached_property`)
-- Keep in mind that RocketPy must be fast!
-
-### Backward Compatibility
-- **Avoid breaking changes** in public APIs
-- Use **deprecation warnings** before removing features
-- **Document code changes** in docstrings and CHANGELOG
-
-## AI Assistant Guidelines
-
-### Code Generation
-- **Always include docstrings** for new functions and classes
-- **Follow existing patterns** in the codebase
-- **Consider edge cases** and error conditions
-
-### Code Review and Suggestions
-- **Check for consistency** with existing code style
-- **Verify physical units** and coordinate systems
-- **Ensure proper error handling** and input validation
-- **Suggest performance improvements** when applicable
-- **Recommend additional tests** for new functionality
-
-### Documentation Assistance
-- **Use NumPy docstring format** consistently
-- **Include practical examples** in docstrings
-- **Document physical meanings** of parameters
-- **Cross-reference related functions** and classes
-
-## Testing Guidelines
-
-### Unit Tests
-- **Test individual methods** in isolation
-- **Use fixtures** from the appropriate test fixture modules
-- **Mock external dependencies** when necessary
-- **Test both happy path and error conditions**
-
-### Integration Tests
-- **Test interactions** between components
-- **Verify end-to-end workflows** (Environment → Motor → Rocket → Flight)
-
-### Test Data
-- **Use realistic parameters** for rocket simulations
-- **Include edge cases** (very small/large rockets, extreme conditions)
-- **Test with different coordinate systems** and orientations
-
-## Project-Specific Considerations
-
-### User Experience
-- **Provide helpful error messages** with context and suggestions
-- **Include examples** in docstrings and documentation
-- **Support common use cases** with reasonable defaults
-
-## Examples of Good Practices
-
-### Function Definition
-```python
-def calculate_drag_force(
-    velocity,
-    air_density,
-    drag_coefficient,
-    reference_area
-):
-    """Calculate drag force using the standard drag equation.
-
-    Parameters
-    ----------
-    velocity : float
-        Velocity magnitude in m/s.
-    air_density : float
-        Air density in kg/m³.
-    drag_coefficient : float
-        Dimensionless drag coefficient.
-    reference_area : float
-        Reference area in m².
-
-    Returns
-    -------
-    float
-        Drag force in N.
-
-    Examples
-    --------
-    >>> drag_force = calculate_drag_force(100, 1.225, 0.5, 0.01)
-    >>> print(f"Drag force: {drag_force:.2f} N")
-    """
-    if velocity < 0:
-        raise ValueError("Velocity must be non-negative")
-    if air_density <= 0:
-        raise ValueError("Air density must be positive")
-    if reference_area <= 0:
-        raise ValueError("Reference area must be positive")
-
-    return 0.5 * air_density * velocity**2 * drag_coefficient * reference_area
-```
-
-### Test Example
-```python
-def test_calculate_drag_force_returns_correct_value():
-    """Test drag force calculation with known inputs."""
-    # Arrange
-    velocity = 100.0  # m/s
-    air_density = 1.225  # kg/m³
-    drag_coefficient = 0.5
-    reference_area = 0.01  # m²
-    expected_force = 30.625  # N
-
-    # Act
-    result = calculate_drag_force(velocity, air_density, drag_coefficient, reference_area)
-
-    # Assert
-    assert abs(result - expected_force) < 1e-6
-```
-
-
-Remember: RocketPy prioritizes accuracy, performance, and usability. Always consider the physical meaning of calculations and provide clear, well-documented interfaces for users.
+# RocketPy Workspace Instructions
+
+## Code Style
+- Use snake_case for variables, functions, methods, and modules. Use descriptive names.
+- Use PascalCase for classes and UPPER_SNAKE_CASE for constants.
+- Keep lines at 88 characters and follow PEP 8 unless existing code in the target file differs.
+- Run Ruff as the source of truth for formatting/import organization:
+  - `make format`
+  - `make lint`
+- Use NumPy-style docstrings for public classes, methods, and functions, including units.
+- In case of tooling drift between docs and config, prefer current repository tooling in `Makefile`
+  and `pyproject.toml`.
+
+## Architecture
+- RocketPy is a modular Python library; keep feature logic in the correct package boundary:
+  - `rocketpy/simulation`: flight simulation and Monte Carlo orchestration.
+  - `rocketpy/rocket`, `rocketpy/motors`, `rocketpy/environment`: domain models.
+  - `rocketpy/mathutils`: numerical primitives and interpolation utilities.
+  - `rocketpy/plots`, `rocketpy/prints`: output and visualization layers.
+- Prefer extending existing classes/patterns over introducing new top-level abstractions.
+- Preserve public API stability in `rocketpy/__init__.py` exports.
+
+## Build and Test
+- Use Makefile targets for OS-agnostic workflows:
+  - `make install`
+  - `make pytest`
+  - `make pytest-slow`
+  - `make coverage`
+  - `make coverage-report`
+  - `make build-docs`
+- Before finishing code changes, run focused tests first, then broader relevant suites.
+- When running Python directly in this workspace, prefer `.venv/Scripts/python.exe`.
+- Slow tests are explicitly marked with `@pytest.mark.slow` and are run with `make pytest-slow`.
+- For docs changes, check `make build-docs` output and resolve warnings/errors when practical.
+
+## Development Workflow
+- Target pull requests to `develop` by default; `master` is the stable branch.
+- Use branch names in `type/description` format, such as:
+  - `bug/<description>`
+  - `doc/<description>`
+  - `enh/<description>`
+  - `mnt/<description>`
+  - `tst/<description>`
+- Prefer rebasing feature branches on top of `develop` to keep history linear.
+- Keep commit and PR titles explicit and prefixed with project acronyms when possible:
+  - `BUG`, `DOC`, `ENH`, `MNT`, `TST`, `BLD`, `REL`, `REV`, `STY`, `DEV`.
+
+## Conventions
+- SI units are the default. Document units and coordinate-system references explicitly.
+- Position/reference-frame arguments are critical in this codebase. Be explicit about orientation
+  (for example, `tail_to_nose`, `nozzle_to_combustion_chamber`).
+- Include unit tests for new behavior. Follow AAA structure and clear test names.
+- Use fixtures from `tests/fixtures`; if adding a new fixture module, update `tests/conftest.py`.
+- Use `pytest.approx` for floating-point checks where appropriate.
+- Use `@cached_property` for expensive computations when helpful, and be careful with stale-cache
+  behavior when underlying mutable state changes.
+- Keep behavior backward compatible across the public API exported via `rocketpy/__init__.py`.
+- Prefer extending existing module patterns over creating new top-level package structure.
+
+## Testing Taxonomy
+- Unit tests are mandatory for new behavior.
+- Unit tests in RocketPy can be sociable (real collaborators allowed) but should still be fast and
+  method-focused.
+- Treat tests as integration tests when they are strongly I/O-oriented or broad across many methods,
+  including `all_info()` convention cases.
+- Acceptance tests represent realistic user/flight scenarios and may compare simulation thresholds to
+  known flight data.
+
+## Documentation Links
+- Contributor workflow and setup: `docs/development/setting_up.rst`
+- Style and naming details: `docs/development/style_guide.rst`
+- Testing philosophy and structure: `docs/development/testing.rst`
+- API reference conventions: `docs/reference/index.rst`
+- Domain/physics background: `docs/technical/index.rst`
+
+## Scoped Customizations
+- Simulation-specific rules: `.github/instructions/simulation-safety.instructions.md`
+- Test-authoring rules: `.github/instructions/tests-python.instructions.md`
+- RST/Sphinx documentation rules: `.github/instructions/sphinx-docs.instructions.md`
+- Specialized review persona: `.github/agents/rocketpy-reviewer.agent.md`
diff --git a/.github/instructions/simulation-safety.instructions.md b/.github/instructions/simulation-safety.instructions.md
new file mode 100644
index 000000000..cc2af5d27
--- /dev/null
+++ b/.github/instructions/simulation-safety.instructions.md
@@ -0,0 +1,41 @@
+---
+description: "Use when editing rocketpy/simulation code, including Flight state updates, Monte Carlo orchestration, post-processing, or cached computations. Covers simulation state safety, unit/reference-frame clarity, and regression checks."
+name: "Simulation Safety"
+applyTo: "rocketpy/simulation/**/*.py"
+---
+# Simulation Safety Guidelines
+
+- Keep simulation logic inside `rocketpy/simulation` and avoid leaking domain behavior that belongs in
+  `rocketpy/rocket`, `rocketpy/motors`, or `rocketpy/environment`.
+- Preserve public API behavior and exported names used by `rocketpy/__init__.py`.
+- Prefer extending existing simulation components before creating new abstractions:
+  - `flight.py`: simulation state, integration flow, and post-processing.
+  - `monte_carlo.py`: orchestration and statistical execution workflows.
+  - `flight_data_exporter.py` and `flight_data_importer.py`: persistence and interchange.
+  - `flight_comparator.py`: comparative analysis outputs.
+- Be explicit with physical units and reference frames in new parameters, attributes, and docstrings.
+- For position/orientation-sensitive behavior, use explicit conventions (for example
+  `tail_to_nose`, `nozzle_to_combustion_chamber`) and avoid implicit assumptions.
+- Treat state mutation carefully when cached values exist.
+- If changes can invalidate `@cached_property` values, either avoid post-computation mutation or
+  explicitly invalidate affected caches in a controlled, documented way.
+- Keep numerical behavior deterministic unless stochastic behavior is intentional and documented.
+- For Monte Carlo and stochastic code paths, make randomness controllable and reproducible when tests
+  rely on it.
+- Prefer vectorized NumPy operations for hot paths and avoid introducing Python loops in
+  performance-critical sections without justification.
+- Guard against numerical edge cases (zero/near-zero denominators, interpolation limits, and boundary
+  conditions).
+- Do not change default numerical tolerances or integration behavior without documenting motivation and
+  validating regression impact.
+- Add focused regression tests for changed behavior, including edge cases and orientation-dependent
+  behavior.
+- For floating-point expectations, use `pytest.approx` with meaningful tolerances.
+- Run focused tests first, then broader relevant tests (`make pytest` and `make pytest-slow` when
+  applicable).
+
+See:
+- `docs/development/testing.rst`
+- `docs/development/style_guide.rst`
+- `docs/development/setting_up.rst`
+- `docs/technical/index.rst`
diff --git a/.github/instructions/sphinx-docs.instructions.md b/.github/instructions/sphinx-docs.instructions.md
new file mode 100644
index 000000000..8c24cac53
--- /dev/null
+++ b/.github/instructions/sphinx-docs.instructions.md
@@ -0,0 +1,32 @@
+---
+description: "Use when writing or editing docs/**/*.rst. Covers Sphinx/reStructuredText conventions, cross-references, toctree hygiene, and RocketPy unit/reference-frame documentation requirements."
+name: "Sphinx RST Conventions"
+applyTo: "docs/**/*.rst"
+---
+# Sphinx and RST Guidelines
+
+- Follow existing heading hierarchy and style in the target document.
+- Prefer linking to existing documentation pages instead of duplicating content.
+- Use Sphinx cross-references where appropriate (`:class:`, `:func:`, `:mod:`, `:doc:`, `:ref:`).
+- Keep API names and module paths consistent with current code exports.
+- Document physical units and coordinate/reference-frame conventions explicitly.
+- Include concise, practical examples when introducing new user-facing behavior.
+- Keep prose clear and technical; avoid marketing language in development/reference docs.
+- When adding a new page, update the relevant `toctree` so it appears in navigation.
+- Use RocketPy docs build workflow:
+  - `make build-docs` from repository root for normal validation.
+  - If stale artifacts appear, clean docs build outputs via `cd docs && make clean`, then rebuild.
+- Treat new Sphinx warnings/errors as issues to fix or explicitly call out in review notes.
+- Keep `docs/index.rst` section structure coherent with user, development, reference, technical, and
+  examples navigation.
+- Do not edit Sphinx-generated scaffolding files unless explicitly requested:
+  - `docs/Makefile`
+  - `docs/make.bat`
+- For API docs, ensure references remain aligned with exported/public objects and current module paths.
+
+See:
+- `docs/index.rst`
+- `docs/development/build_docs.rst`
+- `docs/development/style_guide.rst`
+- `docs/reference/index.rst`
+- `docs/technical/index.rst`
diff --git a/.github/instructions/tests-python.instructions.md b/.github/instructions/tests-python.instructions.md
new file mode 100644
index 000000000..1e9626142
--- /dev/null
+++ b/.github/instructions/tests-python.instructions.md
@@ -0,0 +1,36 @@
+---
+description: "Use when creating or editing pytest files in tests/. Enforces AAA structure, naming conventions, fixture usage, parameterization, slow-test marking, and numerical assertion practices for RocketPy."
+name: "RocketPy Pytest Standards"
+applyTo: "tests/**/*.py"
+---
+# RocketPy Test Authoring Guidelines
+
+- Unit tests are mandatory for new behavior.
+- Follow AAA structure in each test: Arrange, Act, Assert.
+- Use descriptive test names matching project convention:
+  - `test_methodname`
+  - `test_methodname_stateundertest`
+  - `test_methodname_expectedbehaviour`
+- Include docstrings that clearly state expected behavior and context.
+- Prefer parameterization for scenario matrices instead of duplicated tests.
+- Classify tests correctly:
+  - `tests/unit`: fast, method-focused tests (sociable unit tests are acceptable in RocketPy).
+  - `tests/integration`: broad multi-method/component interactions and strongly I/O-oriented cases.
+  - `tests/acceptance`: realistic end-user/flight scenarios with threshold-based expectations.
+- By RocketPy convention, tests centered on `all_info()` behavior are integration tests.
+- Reuse fixtures from `tests/fixtures` whenever possible.
+- Keep fixture organization aligned with existing categories under `tests/fixtures`
+  (environment, flight, motor, rockets, surfaces, units, etc.).
+- If you add a new fixture module, update `tests/conftest.py` so fixtures are discoverable.
+- Keep tests deterministic: set seeds when randomness is involved and avoid unstable external
+  dependencies unless integration behavior explicitly requires them.
+- Use `pytest.approx` for floating-point comparisons with realistic tolerances.
+- Mark expensive tests with `@pytest.mark.slow` and ensure they can run under the project slow-test
+  workflow.
+- Include at least one negative or edge-case assertion for new behaviors.
+- When adding a bug fix, include a regression test that fails before the fix and passes after it.
+
+See:
+- `docs/development/testing.rst`
+- `docs/development/style_guide.rst`
+- `docs/development/setting_up.rst`
diff --git a/.github/renovate.json b/.github/renovate.json
new file mode 100644
index 000000000..1d2808213
--- /dev/null
+++ b/.github/renovate.json
@@ -0,0 +1,42 @@
+{
+  "$schema": "https://docs.renovatebot.com/renovate-schema.json",
+  "extends": [
+    "config:recommended"
+  ],
+  "baseBranches": [
+    "develop"
+  ],
+  "labels": [
+    "dependencies"
+  ],
+  "dependencyDashboard": true,
+  "automerge": false,
+  "pip-compile": {
+    "managerFilePatterns": [
+      "/^docs/requirements\\.txt$/"
+    ]
+  },
+  "packageRules": [
+    {
+      "matchPackagePatterns": [
+        "*"
+      ],
+      "matchUpdateTypes": [
+        "minor",
+        "patch"
+      ],
+      "groupName": "all non-major dependencies",
+      "groupSlug": "all-non-major"
+    },
+    {
+      "description": "docs/requirements.txt is autogenerated by pip-compile from docs/requirements.in. Let the pip-compile manager regenerate the lock file, and stop the pip_requirements manager from editing the autogenerated file line by line.",
+      "matchManagers": [
+        "pip_requirements"
+      ],
+      "matchFileNames": [
+        "docs/requirements.txt"
+      ],
+      "enabled": false
+    }
+  ]
+}
diff --git a/.github/workflows/changelog.yml b/.github/workflows/changelog.yml
new file mode 100644
index 000000000..7bf27daf7
--- /dev/null
+++ b/.github/workflows/changelog.yml
@@ -0,0 +1,83 @@
+name: Populate Changelog
+on:
+  pull_request:
+    types: [closed]
+    branches:
+      - develop
+
+permissions:
+  contents: write
+
+jobs:
+  Changelog:
+    if: github.event.pull_request.merged == true
+    runs-on: ubuntu-latest
+
+    steps:
+      - name: Clone RocketPy
+        uses: actions/checkout@v4
+        with:
+          repository: RocketPy-Team/RocketPy
+          ref: develop
+          token: ${{ secrets.RELEASE_TOKEN }}
+
+      - name: Update Changelog
+        env:
+          PR_TITLE: ${{ github.event.pull_request.title }}
+          PR_NUMBER: ${{ github.event.pull_request.number }}
+          PR_LABELS: ${{ join(github.event.pull_request.labels.*.name, ',') }}
+        run: |
+          # The PR title is untrusted input, so it is read from the environment
+          # inside Python rather than interpolated into a shell/sed program.
+          # This avoids both shell injection and sed breaking on special
+          # characters (\, /, &, newlines) in the title.
+          python - <<'PY'
+          import os
+
+          labels = os.environ.get("PR_LABELS", "")
+          title = os.environ["PR_TITLE"]
+          number = os.environ["PR_NUMBER"]
+
+          section, prefix = "### Added", "ENH"
+          if "Bug" in labels:
+              section, prefix = "### Fixed", "BUG"
+          elif "Refactor" in labels:
+              section, prefix = "### Changed", "MNT"
+          elif "Docs" in labels and "Git housekeeping" in labels:
+              section, prefix = "### Changed", "DOC"
+          elif "Tests" in labels:
+              section, prefix = "### Changed", "TST"
+          elif "Docs" in labels:
+              section, prefix = "### Added", "DOC"
+
+          entry = (
+              f"- {prefix}: {title} "
+              f"[#{number}](https://github.com/RocketPy-Team/RocketPy/pull/{number})\n"
+          )
+
+          with open("CHANGELOG.md", encoding="utf-8") as handle:
+              lines = handle.readlines()
+
+          for index, line in enumerate(lines):
+              if line.rstrip("\n") == section:
+                  insert_at = index + 1
+                  # Place the entry at the top of the list, after the single
+                  # blank line that follows the section header.
+                  if insert_at < len(lines) and lines[insert_at].strip() == "":
+                      insert_at += 1
+                  lines.insert(insert_at, entry)
+                  break
+          else:
+              raise SystemExit(f"Section {section!r} not found in CHANGELOG.md")
+
+          with open("CHANGELOG.md", "w", encoding="utf-8") as handle:
+              handle.writelines(lines)
+          PY
+
+      - name: Push Changes
+        run: |
+          git config user.name "github-actions[bot]"
+          git config user.email "github-actions[bot]@users.noreply.github.com"
+          git add CHANGELOG.md
+          git commit -m "DOC: Update Changelog for PR #${{ github.event.pull_request.number }}"
+          git push
diff --git a/.github/workflows/docs.yml b/.github/workflows/docs.yml
new file mode 100644
index 000000000..806bef0dc
--- /dev/null
+++ b/.github/workflows/docs.yml
@@ -0,0 +1,107 @@
+name: Documentation
+
+on:
+  # Only PRs targeting master (base branch = master) and pushes to master.
+  pull_request:
+    types: [opened, synchronize, reopened, ready_for_review]
+    branches: [master]
+    paths:
+      - "docs/**"
+      - "rocketpy/**" # docstrings feed the autodoc API reference
+      - "pyproject.toml"
+      - "requirements*"
+      - ".readthedocs.yaml"
+      - ".github/workflows/docs.yml"
+  push:
+    branches: [master]
+    paths:
+      - "docs/**"
+      - "rocketpy/**"
+      - "pyproject.toml"
+      - "requirements*"
+      - ".readthedocs.yaml"
+      - ".github/workflows/docs.yml"
+
+# Least privilege: this workflow only needs to read the repository.
+permissions:
+  contents: read
+
+defaults:
+  run:
+    shell: bash
+
+jobs:
+  build-docs:
+    runs-on: ubuntu-latest
+    strategy:
+      matrix:
+        python-version: ["3.12"] # match the Read the Docs build environment
+    env:
+      MPLBACKEND: Agg
+      # Render jupyter-execute cells as static code blocks instead of running
+      # them. This keeps the check fast and deterministic: no simulations and,
+      # crucially, no live network calls to external weather/data servers (which
+      # make the full build slow and flaky). Read the Docs still executes the
+      # cells to render live outputs; this job only validates the docs structure
+      # (reStructuredText, cross-references, toctrees, autodoc API reference).
+      DOCS_SKIP_EXECUTE: "1"
+    steps:
+      - uses: actions/checkout@v4
+
+      - name: Install pandoc (required by nbsphinx)
+        run: sudo apt-get update && sudo apt-get install -y pandoc
+
+      - name: Set up Python ${{ matrix.python-version }}
+        uses: actions/setup-python@v5
+        with:
+          python-version: ${{ matrix.python-version }}
+          cache: "pip"
+          cache-dependency-path: |
+            docs/requirements.txt
+            requirements.txt
+
+      - name: Install dependencies (mirrors .readthedocs.yaml)
+        run: |
+          python -m pip install --upgrade pip
+          pip install -r docs/requirements.txt
+          pip install -r requirements.txt
+          pip install .[all]
+
+      - name: Cache Sphinx doctrees
+        uses: actions/cache@v4
+        with:
+          path: docs/_build/doctrees
+          key: sphinx-doctrees-${{ github.ref }}-${{ hashFiles('docs/**', 'rocketpy/**') }}
+          restore-keys: |
+            sphinx-doctrees-${{ github.ref }}-
+            sphinx-doctrees-
+
+      - name: Build docs (warnings-as-errors)
+        working-directory: docs
+        run: |
+          sphinx-build -b html -W --keep-going \
+            -d _build/doctrees \
+            -w _build/sphinx-warnings.txt \
+            . _build/html
+
+      - name: Surface Sphinx warnings as annotations
+        if: always()
+        run: |
+          if [ -s docs/_build/sphinx-warnings.txt ]; then
+            echo "::group::Sphinx warnings"
+            cat docs/_build/sphinx-warnings.txt
+            echo "::endgroup::"
+            while IFS= read -r line; do
+              echo "::warning::${line}"
+            done < docs/_build/sphinx-warnings.txt
+          else
+            echo "No Sphinx warnings 🎉"
+          fi
+
+      - name: Upload built HTML
+        if: always()
+        uses: actions/upload-artifact@v4
+        with:
+          name: docs-html
+          path: docs/_build/html
+          if-no-files-found: error
diff --git a/.pylintrc b/.pylintrc
index b0aaf655c..c76a6d459 100644
--- a/.pylintrc
+++ b/.pylintrc
@@ -225,6 +225,11 @@ good-names=FlightPhases,
            center_of_mass_without_motor_to_CDM,
            motor_center_of_dry_mass_to_CDM,
            generic_motor_cesaroni_M1520,
+           R_phi,
+           R_delta, 
+           R_pi,
+           R_uncanted,
+           R_body_to_fin, 
            Re, # Reynolds number
 
 # Good variable names regexes, separated by a comma. If names match any regex,
@@ -385,7 +390,7 @@ indent-string='    '
 max-line-length=88
 
 # Maximum number of lines in a module.
-max-module-lines=3000
+max-module-lines=3050
 
 # Allow the body of a class to be on the same line as the declaration if body
 # contains single statement.
diff --git a/CHANGELOG.md b/CHANGELOG.md
index 183479c4b..fd1fe4c64 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -32,15 +32,64 @@ Attention: The newest changes should be on top -->
 
 ### Added
 
--
+### Changed
+
+### Fixed
+
+
+## [v1.13.0] - 2026-07-04
+
+### Added
+
+- ENH: FIX: pre release hardening [#1047](https://github.com/RocketPy-Team/RocketPy/pull/1047)
+- ENH: DEV: Claude Code ruff hooks (auto-format on edit + pre-push lint guard) [#1046](https://github.com/RocketPy-Team/RocketPy/pull/1046)
+- ENH: CI: create a CI for testing docs updates + solve different docs issues [#1045](https://github.com/RocketPy-Team/RocketPy/pull/1045)
+- ENH: MNT: final fixes before next release [#1044](https://github.com/RocketPy-Team/RocketPy/pull/1044)
+- ENH: Individual Fins: add `Fin`, `TrapezoidalFin`, `EllipticalFin`, and `FreeFormFin` classes for modeling asymmetric or individually-positioned fins [#818](https://github.com/RocketPy-Team/RocketPy/pull/818)
+- ENH: Add AIGFS and HRRR forecast models to the Environment class [#951](https://github.com/RocketPy-Team/RocketPy/pull/951)
+- ENH: Add RingClusterMotor for annular clustered motor modeling [#924](https://github.com/RocketPy-Team/RocketPy/pull/924)
+- ENH: Discrete and Continuous Controllers [#946](https://github.com/RocketPy-Team/RocketPy/pull/946)
+- ENH: Add custom exceptions and unstable rocket warning [#970](https://github.com/RocketPy-Team/RocketPy/pull/970)
+- ENH: Adopt built-in Python logging instead of print() calls (closes [#450](https://github.com/RocketPy-Team/RocketPy/issues/450)) [#973](https://github.com/RocketPy-Team/RocketPy/pull/973)
+- ENH: Pass acceleration (`u_dot`) data to parachute trigger functions [#911](https://github.com/RocketPy-Team/RocketPy/pull/911)
+- ENH: Add 3D flight trajectory and attitude animations in Flight plots layer [#909](https://github.com/RocketPy-Team/RocketPy/pull/909)
+- ENH: Monte Carlo Formatting Options [#947](https://github.com/RocketPy-Team/RocketPy/pull/947)
+- ENH: Adaptive Monte Carlo via Convergence Criteria [#922](https://github.com/RocketPy-Team/RocketPy/pull/922)
+- ENH: Auto-Detection of Pressure Conversion Factor [#966](https://github.com/RocketPy-Team/RocketPy/pull/966)
+- ENH: Introduce pressure unit conversion when using forecast/reanalysis/ensemble data [#955](https://github.com/RocketPy-Team/RocketPy/pull/955)
+- MNT: Refactor parachute implementation with abstract base and hemispherical model split [#958](https://github.com/RocketPy-Team/RocketPy/pull/958)
+- DOC: Add aerodynamic surfaces user guide [#1043](https://github.com/RocketPy-Team/RocketPy/pull/1043)
+- DOC: Add Valkyrie flight example (Bisky Team) [#967](https://github.com/RocketPy-Team/RocketPy/pull/967)
+- DOC: Configure AI instructions and update developer docs [#975](https://github.com/RocketPy-Team/RocketPy/pull/975)
+- ENH: Auto Populate Changelog [#919](https://github.com/RocketPy-Team/RocketPy/pull/919)
+- MNT: Sync develop's Renovate config with master (#1039) [#1040](https://github.com/RocketPy-Team/RocketPy/pull/1040)
+- MNT: Configure Renovate Bot targeting develop branch [#972](https://github.com/RocketPy-Team/RocketPy/pull/972)
 
 ### Changed
 
-- 
+- REL: bumps up rocketpy version to 1.13.0 [#1048](https://github.com/RocketPy-Team/RocketPy/pull/1048)
+- MNT: **Breaking**: `Parachute` is now an abstract base class and can no longer be instantiated directly; use `HemisphericalParachute` (or `Rocket.add_parachute`, which builds it for you). Loading old serialized files still works [#958](https://github.com/RocketPy-Team/RocketPy/pull/958)
+- MNT: Discrete controllers are now called exactly once per time node (previously twice); results may change for stateful controllers and `observed_variables` no longer contains duplicated entries [#949](https://github.com/RocketPy-Team/RocketPy/pull/949)
+- MNT: Multi-dimensional linear `Function` objects now apply their extrapolation rule to points outside the data's convex hull (previously returned NaN) [#969](https://github.com/RocketPy-Team/RocketPy/pull/969)
+- MNT: Informational messages previously shown with `print()` now use Python logging and are silent by default; call `rocketpy.utils.enable_logging()` to see them [#973](https://github.com/RocketPy-Team/RocketPy/pull/973)
+
+### Deprecated
+
+- MNT: Rename `radius` to `radius_function` in `CylindricalTank` and `SphericalTank`; old `radius=` keyword argument now raises `DeprecationWarning` [#957](https://github.com/RocketPy-Team/RocketPy/pull/957)
+
+### Removed
+
+- MNT: Remove redundant, unused per-level `wind_heading`/`wind_direction` functions from `EnvironmentAnalysis` pressure-level data (derivable from `wind_velocity_x`/`wind_velocity_y`) [#1041](https://github.com/RocketPy-Team/RocketPy/pull/1041)
 
 ### Fixed
 
--
+- BUG: fix individual fin (`TrapezoidalFin`, `EllipticalFin`, `FreeFormFin`) serialization crash when saving rockets/flights [#1048](https://github.com/RocketPy-Team/RocketPy/pull/1048)
+- BUG: support the new Wyoming sounding WSGI page format (legacy cgi-bin endpoint was discontinued by UWyo) [#1048](https://github.com/RocketPy-Team/RocketPy/pull/1048)
+- FIX: pre-release hardening — bug fixes across the unreleased features [#1047](https://github.com/RocketPy-Team/RocketPy/pull/1047)
+- BUG: Remove duplicate controller process; controllers were being invoked twice per time node [#949](https://github.com/RocketPy-Team/RocketPy/pull/949)
+- BUG: fix wind heading and direction wraparound interpolation [#974](https://github.com/RocketPy-Team/RocketPy/pull/974)
+- BUG: fix NaN in ND linear interpolation outside convex hull (closes [#926](https://github.com/RocketPy-Team/RocketPy/issues/926)) [#969](https://github.com/RocketPy-Team/RocketPy/pull/969)
+- BUG: Add wraparound logic for wind direction in environment plots [#939](https://github.com/RocketPy-Team/RocketPy/pull/939)
 
 ## [v1.12.1] - 2026-04-03
 
@@ -78,17 +127,16 @@ Attention: The newest changes should be on top -->
 
 ### Fixed
 
-- BUG: Restore `Rocket.power_off_drag` and `Rocket.power_on_drag` as `Function` objects while preserving raw inputs in `power_off_drag_input` and `power_on_drag_input` [#941](https://github.com/RocketPy-Team/RocketPy/pull/941)
-- BUG: Add explicit timeouts to ThrustCurve API requests [#935](https://github.com/RocketPy-Team/RocketPy/pull/935)
 - BUG: Fix hard-coded radius value for parachute added mass calculation [#889](https://github.com/RocketPy-Team/RocketPy/pull/889)
+- BUG: Fix incorrect Jacobian in `only_radial_burn` branch of `SolidMotor.evaluate_geometry` [#944](https://github.com/RocketPy-Team/RocketPy/pull/944)
+- ENH: Restore `power_off_drag`/`power_on_drag` as `Function` objects and preserve raw user input in `_input` attributes [#941](https://github.com/RocketPy-Team/RocketPy/pull/941)
+- ENH: Add explicit timeouts to ThrustCurve API requests [#940](https://github.com/RocketPy-Team/RocketPy/pull/940)
 - DOC: Fix documentation build [#908](https://github.com/RocketPy-Team/RocketPy/pull/908)
 - BUG: energy_data plot not working for 3 dof sims [[#906](https://github.com/RocketPy-Team/RocketPy/issues/906)]
 - BUG: Fix CSV column header spacing in FlightDataExporter [#864](https://github.com/RocketPy-Team/RocketPy/issues/864)
 - BUG: Fix parallel Monte Carlo simulation showing incorrect iteration count [#806](https://github.com/RocketPy-Team/RocketPy/pull/806)
 - BUG: Fix missing titles in roll parameter plots for fin sets [#934](https://github.com/RocketPy-Team/RocketPy/pull/934)
 - BUG: Duplicate _controllers in Flight.TimeNodes.merge() [#931](https://github.com/RocketPy-Team/RocketPy/pull/931)
-- BUG: Fix incorrect Jacobian in `only_radial_burn` branch of `SolidMotor.evaluate_geometry` [#935](https://github.com/RocketPy-Team/RocketPy/pull/935)
-- BUG: Add explicit timeouts to ThrustCurve API requests [#935](https://github.com/RocketPy-Team/RocketPy/pull/935)
 
 ## [v1.11.0] - 2025-11-01
 
diff --git a/README.md b/README.md
index 8247ab1a3..8a3a4b651 100644
--- a/README.md
+++ b/README.md
@@ -143,7 +143,7 @@ The following image shows how the four main classes interact with each other:
 A typical workflow starts with importing these classes from RocketPy:
 
 ```python
-from rocketpy import Environment, Rocket, SolidMotor, Flight
+from rocketpy import Environment, Rocket, SolidMotor, Flight, HemisphericalParachute
 ```
 
 An optional step is to import datetime, which is used to define the date of the simulation:
@@ -255,7 +255,7 @@ tail = calisto.add_tail(
 You may want to add parachutes to your rocket as well:
 
 ```python
-main = calisto.add_parachute(
+main = HemisphericalParachute(
     name="main",
     cd_s=10.0,
     trigger=800,  # ejection altitude in meters
@@ -267,7 +267,7 @@ main = calisto.add_parachute(
     porosity=0.0432,
 )
 
-drogue = calisto.add_parachute(
+drogue = HemisphericalParachute(
     name="drogue",
     cd_s=1.0,
     trigger="apogee",  # ejection at apogee
@@ -278,6 +278,9 @@ drogue = calisto.add_parachute(
     height=1.5,
     porosity=0.0432,
 )
+
+calisto.add_parachute(parachute = main)
+calisto.add_parachute(parachute = drogue)
 ```
 
 Finally, you can create a Flight object to simulate your trajectory. To get help on the Flight class, use:
@@ -310,10 +313,12 @@ Here is just a quick taste of what RocketPy is able to calculate. There are hund
 
 ![6-DOF Trajectory Plot](https://raw.githubusercontent.com/RocketPy-Team/RocketPy/master/docs/static/rocketpy_example_trajectory.svg)
 
-If you want to see the trajectory on Google Earth, RocketPy acn easily export a KML file for you:
+If you want to see the trajectory on Google Earth, RocketPy can easily export a KML file for you:
 
 ```python
-test_flight.export_kml(file_name="test_flight.kml")
+from rocketpy.simulation import FlightDataExporter
+
+FlightDataExporter(test_flight).export_kml(file_name="test_flight.kml")
 ```
 
 <img alt="6-DOF Trajectory Plot" src="https://raw.githubusercontent.com/RocketPy-Team/RocketPy/master/docs/static/trajectory-earth.png" width="501">
diff --git a/data/motors/cesaroni/Cesaroni_1997K650-21A.eng b/data/motors/cesaroni/Cesaroni_1997K650-21A.eng
new file mode 100644
index 000000000..e95c47090
--- /dev/null
+++ b/data/motors/cesaroni/Cesaroni_1997K650-21A.eng
@@ -0,0 +1,12 @@
+;Pink 54mm 5G
+;1997-K650-PK-21
+1997-K650-PK-21 54 488 21-19-17-15-13-11 1.0651 1.71 CTI 
+0.011 1353.5
+0.028 793.832
+0.186 815.421
+2.578 601.186
+2.689 479.953
+2.855 189.324
+3.086 43.179
+3.451 0
+;
\ No newline at end of file
diff --git a/data/rockets/valkyrie/Dima.json b/data/rockets/valkyrie/Dima.json
new file mode 100644
index 000000000..048ba3c74
--- /dev/null
+++ b/data/rockets/valkyrie/Dima.json
@@ -0,0 +1,38 @@
+{
+  "launch": {
+    "rail_length": {
+      "value": 10,
+      "dispersion": 0.001
+    },
+    "ensemble_member": null
+  },
+  "Environment": {
+    "latitude": {
+      "value": 43.077771
+    },
+    "longitude": {
+      "value": -2.684446
+    },
+    "elevation": {
+      "value": 592
+    },
+    "max_expected_height": {
+      "value": 3000
+    },
+    "timezone": "Europe/Madrid"
+  },
+  "Montecarlo": {
+    "map_filename": "Dima.PNG",
+    "map_scale": 1,
+    "append": false,
+    "map_limits": [
+      -20000,
+      20000,
+      -20000,
+      20000
+    ]
+  },
+  "Flight": {
+    "max_time": 3000
+  }
+}
diff --git a/data/rockets/valkyrie/VLK.json b/data/rockets/valkyrie/VLK.json
new file mode 100644
index 000000000..92318f469
--- /dev/null
+++ b/data/rockets/valkyrie/VLK.json
@@ -0,0 +1,76 @@
+{
+    "VLK": {
+        "rocket": {
+            "rocket_mass":              {"value": 5.65, "dispersion": 0.2},
+            "rocket_center_of_mass_without_motor":          {"value": 0.844, "dispersion": 0.01},
+            "rocket_coordinate_system_orientation":         "tail_to_nose",
+            "rocket_inertia_11":        {"value": 1.806, "dispersion": 0.1},
+            "rocket_inertia_33":        {"value": 0.0183, "dispersion": 0.001},
+            "rocket_radius":            {"value": 0.055, "dispersion": 0.0001},
+            "motor_position":           {"value": 0, "dispersion": 0}
+        },
+        "motor": {
+            "motor_coordinate_system_orientation":      "nozzle_to_combustion_chamber",
+            "motor_thrust_source":              "./data/motors/cesaroni/Cesaroni_1997K650-21A.eng",
+            "motor_dry_mass":                   {"value": 0.6449, "dispersion": 0.001},
+            "motor_inertia_11":                 {"value": 0.0343, "dispersion": 0.0001},
+            "motor_inertia_33":                 {"value": 0.0008, "dispersion": 0.0001},
+            "motor_dry_mass_position":          {"value": 0.246, "dispersion": 0.001},
+            "motor_impulse":                    {"value": 2300, "dispersion": 20},
+            "motor_burn_time":                  {"value": 3.5, "dispersion": 0.1},
+            "nozzle_radius":                    {"value": 0.045, "dispersion": 0.0005},
+            "nozzle_position":                  {"value": 0},
+            "throat_radius":                    {"value": 0.023, "dispersion": 0.0005},
+            "grain_number":                     {"value": 5},
+            "grain_separation":                 {"value": 0.001, "dispersion": 0.0001},
+            "grain_density":                    {"value": 1170, "dispersion": 10},
+            "grain_outer_radius":               {"value": 0.025, "dispersion": 0.001},
+            "grain_initial_inner_radius":       {"value": 0.01, "dispersion": 0.000375},
+            "grain_initial_height":             {"value": 0.0966, "dispersion": 0.001},
+            "grains_center_of_mass_position":   {"value": 0.246, "dispersion": 0.003},
+            "power_off_drag":                   {"value": 0.35, "dispersion": 0.05},
+            "power_on_drag":                    {"value": 0.35, "dispersion": 0.05}
+        },
+        "nose": {
+            "nose_length":          {"value": 0.20, "dispersion": 0.01},
+            "nose_kind":            "elliptical",
+            "nose_power":           {"value": null, "dispersion": null},
+            "nose_position":        {"value": 1.84, "dispersion": 0}
+        },
+        "fins": {
+            "fin_span":                 {"value": 0.0768, "dispersion": 0.001},
+            "fin_root_chord":           {"value": 0.17, "dispersion": 0.005},
+            "fin_tip_chord":            {"value": 0.14, "dispersion": 0.005},
+            "fin_sweep_length":         {"value": 0.10, "dispersion": 0.003},
+            "fin_airfoil":              "None",
+            "fin_position":             {"value": 0.148, "dispersion": 0.001},
+            "fin_cant_angle":           {"value": 0, "dispersion": 0},
+            "fin_n":                    {"value": 4, "dispersion": 0}
+        },
+        "tail": {
+            "top_radius":           {"value": 0.055, "dispersion": 0.001},
+            "bottom_radius":        {"value": 0.03, "dispersion": 0.005},
+            "length":               {"value": 0.15, "dispersion": 0.005},
+            "position":             {"value": 0, "dispersion": 0}
+        },
+        "main_chute": {
+            "cd_s_main":                {"value": 5.786483801, "dispersion": 0.07},
+            "main_lag":                 {"value": 1.73, "dispersion": 0.4},
+            "main_sampling_rate":       {"value": 105},
+            "Funcion de Deploy":        {"value": 0},
+            "main_noise":               [0, 8.3, 0.5]
+        },
+        "drogue_chute": {
+            "cd_s_drogue":              {"value": 0.258940616, "dispersion": 0.07},
+            "drogue_lag":               {"value": 1.73, "dispersion": 0.4},
+            "drogue_sampling_rate":     {"value": 105},
+            "Funcion de Deploy":        {"value": 0},
+            "drogue_noise":             [0, 8.3, 0.5]
+        },
+        "rail_buttons": {
+            "upper_button_position":        {"value": 1.13, "dispersion": 0},
+            "lower_button_position":        {"value": 0.383, "dispersion": 0},
+            "rail_angular_position":        {"value": 0, "dispersion": 0}
+        }
+    }
+}
\ No newline at end of file
diff --git a/data/rockets/valkyrie/flightInfo_merged.csv b/data/rockets/valkyrie/flightInfo_merged.csv
new file mode 100644
index 000000000..521103f73
--- /dev/null
+++ b/data/rockets/valkyrie/flightInfo_merged.csv
@@ -0,0 +1,12579 @@
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diff --git a/docs/conf.py b/docs/conf.py
index 1bbdd7058..4779e5d5f 100644
--- a/docs/conf.py
+++ b/docs/conf.py
@@ -27,7 +27,7 @@
 author = "RocketPy Team"
 
 # The full version, including alpha/beta/rc tags
-release = "1.12.1"
+release = "1.13.0"
 
 
 # -- General configuration ---------------------------------------------------
@@ -67,6 +67,18 @@
     "allow_errors": True,  # Continue building even if cells raise errors
 }
 
+# When DOCS_SKIP_EXECUTE=1, ``jupyter-execute`` directives are rendered as
+# static (non-executing) code blocks instead of running live code. This makes
+# structural doc builds fast and deterministic (no simulations, no network),
+# which is what the GitHub Actions docs check relies on. Read the Docs leaves
+# this unset, so it still executes the cells and renders their live outputs.
+skip_jupyter_execute = os.environ.get("DOCS_SKIP_EXECUTE") == "1"
+
+# Some notebook cells use IPython shell escapes (e.g. ``!pip install rocketpy``)
+# which the Pygments Python lexer cannot tokenize. These are purely cosmetic
+# syntax-highlighting failures, so don't let them fail a warnings-as-errors build.
+suppress_warnings = ["misc.highlighting_failure"]
+
 # Add any paths that contain templates here, relative to this directory.
 templates_path = ["_templates"]
 
@@ -150,3 +162,46 @@
 html_file_suffix = ".html"
 
 htmlhelp_basename = "rocketpy"
+
+
+def setup(app):
+    """Sphinx entry point for optional build-time customizations."""
+    if skip_jupyter_execute:
+        from docutils.parsers.rst import directives
+        from sphinx.directives.code import CodeBlock
+
+        class StaticJupyterExecute(CodeBlock):
+            """Render ``jupyter-execute`` as a non-executing Python code block.
+
+            Accepts (and ignores) the ``jupyter-execute`` directive options so
+            existing pages parse unchanged, but produces a plain highlighted
+            code block instead of a live-executed cell.
+            """
+
+            required_arguments = 0
+            optional_arguments = 1
+            option_spec = dict(CodeBlock.option_spec)
+            option_spec.update(
+                {
+                    "hide-code": directives.flag,
+                    "hide-output": directives.flag,
+                    "code-below": directives.flag,
+                    "stderr": directives.flag,
+                    "raises": directives.unchanged,
+                }
+            )
+
+            def run(self):
+                for key in (
+                    "hide-code",
+                    "hide-output",
+                    "code-below",
+                    "stderr",
+                    "raises",
+                ):
+                    self.options.pop(key, None)
+                if not self.arguments:
+                    self.arguments = ["python3"]
+                return super().run()
+
+        app.add_directive("jupyter-execute", StaticJupyterExecute, override=True)
diff --git a/docs/development/first_pr.rst b/docs/development/first_pr.rst
index 5f3eb876c..c0b07e7f1 100644
--- a/docs/development/first_pr.rst
+++ b/docs/development/first_pr.rst
@@ -96,14 +96,13 @@ The CHANGELOG file
 ------------------
 
 We keep track of the changes in the ``CHANGELOG.md`` file.
-When you open a PR, you should add a new entry to the "Unreleased" section of the file.
-This entry should simply be the title of your PR.
+When you open a PR, you should see the "Unreleased" section of the file.
+An entry will simply contain the title of your PR if merged.
 
 .. note::
 
-    In the future we would like to automate the CHANGELOG update, but for now \
-    it is a manual process, unfortunately.
-
+    The CHANGELOG is auto-updated once a PR is merged based on the associated labels, \
+    which are assigned by the maintainers.
 
 The review process
 ------------------
diff --git a/docs/development/pro_tips.rst b/docs/development/pro_tips.rst
index 465ff7982..9ff491c4b 100644
--- a/docs/development/pro_tips.rst
+++ b/docs/development/pro_tips.rst
@@ -53,13 +53,25 @@ productive.
 Code assistance
 ---------------
 
-Artificial Intelligence (AI) assistance has becoming more and more common in
+Artificial Intelligence (AI) assistance has become more and more common in
 software development.
 Some editors have AI assistance built-in.
-Famous options are GitHub Copilot, JetBrains AI and TabNine.
-
-At this repo, the use of AI tools is welcome, we don't have any restrictions
-against it.
+Famous options are Google Antigravity, GitHub Copilot, Claude Code,
+JetBrains AI, and TabNine.
+
+In this repository, the use of AI tools is welcome; we don't have any
+restrictions against it. To help AI tools perform better and follow our
+standards, we provide pre-configured instructions and skill files within
+the repository:
+
+* **GitHub Copilot**: Uses ``.github/copilot-instructions.md`` (general
+  codebase rules).
+* **Google Antigravity**: Uses the ``.agents/`` folder, containing general
+  workspace rules (``.agents/AGENTS.md``) and contextual workflows
+  (``.agents/skills/``) for simulation safety, test authoring,
+  documentation, and code review.
+* **Claude / Claude Code**: Permissions configured via
+  ``.claude/settings.json``.
 
 A few possible applications of AI tools are:
 
@@ -69,11 +81,9 @@ A few possible applications of AI tools are:
 
 .. tip::
 
-    As of today, November 2024, GitHub Copilot still provides free access for \
-    university email addresses. We can't guarantee this will still be the case \
-    when you are reading this, so check the GitHub Copilot website for more \
-    information.
-
+    Using these pre-configured rules ensures that your AI assistant adheres
+    to RocketPy's style guides (snake_case, NumPy docstrings, 88-char line
+    limits) and testing conventions (AAA structure).
 
 If you are against the use of AI tools, do not worry, you can still contribute
 to the project without using them.
diff --git a/docs/development/style_guide.rst b/docs/development/style_guide.rst
index 510a49560..15a80e5e4 100644
--- a/docs/development/style_guide.rst
+++ b/docs/development/style_guide.rst
@@ -162,15 +162,16 @@ Standard acronyms to start the commit message with are::
 Pull Requests
 ^^^^^^^^^^^^^
 
-When opening a Pull Request, the name of the PR should be clear and concise.
-Similarly to the commit messages, the PR name should start with an acronym indicating the type of PR
-and then a brief description of the changes.
+When opening a Pull Request, the title should be clear and concise.
+It should contain only a brief desctiption of the changes without the acronym (e.g. ENH:, BUG:).
+The maintainers will label your PR accordingly, which will add a prefix via a workflow to indicate 
+type of the PR in the CHANGELOG file.
 
 Here is an example of a good PR name:
 
-- ``BUG: fix the Frequency Response plot of the Flight class``
+- ``fix the Frequency Response plot of the Flight class``
 
-The PR description explain the changes and motivation behind them. There is a template \
+The PR description explains the changes and motivation behind them. There is a template \
 available when opening a PR that can be used to guide you through the process of both \
 describing the changes and making sure all the necessary steps were taken. Of course, \
 you can always modify the template or add more information if you think it is necessary.
diff --git a/docs/development/testing.rst b/docs/development/testing.rst
index fd521167b..e84fde2a2 100644
--- a/docs/development/testing.rst
+++ b/docs/development/testing.rst
@@ -257,8 +257,7 @@ Consider the following integration test:
         """
         # TODO:: this should be added to the set_atmospheric_model() method as a
         #        "file" option, instead of receiving the URL as a string.
-        URL = "http://weather.uwyo.edu/cgi-bin/sounding?region=samer&TYPE=TEXT%3ALIST&YEAR=2019&MONTH=02&FROM=0500&TO=0512&STNM=83779"
-        # give it at least 5 times to try to download the file
+        URL = "https://weather.uwyo.edu/wsgi/sounding?datetime=2019-02-05+00:00:00&id=83779&type=TEXT:LIST"
         example_plain_env.set_atmospheric_model(type="wyoming_sounding", file=URL)
 
         assert example_plain_env.all_info() is None
@@ -267,7 +266,7 @@ Consider the following integration test:
             abs(example_plain_env.barometric_height(example_plain_env.pressure(0)) - 722.0)
             < 1e-8
         )
-        assert abs(example_plain_env.wind_velocity_x(0) - -2.9005178894925043) < 1e-8
+        assert abs(example_plain_env.wind_velocity_x(0) - -2.9130471244363165) < 1e-8
         assert abs(example_plain_env.temperature(100) - 291.75) < 1e-8
 
 This test contains two fundamental traits which defines it as an integration test:
diff --git a/docs/examples/andromeda_flight_sim.ipynb b/docs/examples/andromeda_flight_sim.ipynb
index 9126045b9..7ea8a9d05 100644
--- a/docs/examples/andromeda_flight_sim.ipynb
+++ b/docs/examples/andromeda_flight_sim.ipynb
@@ -37,7 +37,14 @@
    "source": [
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")\n",
     "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
@@ -258,7 +265,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 64,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -276,13 +283,15 @@
     "    position=0.3546,\n",
     ")\n",
     "\n",
-    "Drogue = Andromeda.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\", cd_s=0.84665922014, trigger=\"apogee\", sampling_rate=100, lag=0\n",
     ")\n",
     "\n",
-    "Main = Andromeda.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    \"Main\", cd_s=8.362919643856031, trigger=500, sampling_rate=100, lag=0\n",
-    ")"
+    ")\n",
+    "Andromeda.add_parachute(parachute=Drogue)\n",
+    "Andromeda.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/bella_lui_flight_sim.ipynb b/docs/examples/bella_lui_flight_sim.ipynb
index c6aa685e8..11fe86553 100644
--- a/docs/examples/bella_lui_flight_sim.ipynb
+++ b/docs/examples/bella_lui_flight_sim.ipynb
@@ -31,7 +31,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 9,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -40,7 +40,14 @@
     "import numpy as np\n",
     "from scipy.signal import savgol_filter\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor"
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")"
    ]
   },
   {
@@ -422,18 +429,19 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 44,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Drogue = bella_lui.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=parameters.get(\"CdS_drogue\")[0],\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=105,\n",
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "bella_lui.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/camoes_flight_sim.ipynb b/docs/examples/camoes_flight_sim.ipynb
index 12278daf2..44fac3613 100644
--- a/docs/examples/camoes_flight_sim.ipynb
+++ b/docs/examples/camoes_flight_sim.ipynb
@@ -52,6 +52,7 @@
     "    Environment,\n",
     "    Flight,\n",
     "    Function,\n",
+    "    HemisphericalParachute,\n",
     "    Rocket,\n",
     "    SolidMotor,\n",
     ")\n",
@@ -299,7 +300,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 85,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -307,9 +308,10 @@
     "    return True if y[5] < 5 and y[2] > 300 else False\n",
     "\n",
     "\n",
-    "Drogue = CAMOES.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\", cd_s=0.33, sampling_rate=400, lag=1.5, trigger=drogue_trigger\n",
-    ")"
+    ")\n",
+    "CAMOES.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/defiance_flight_sim.ipynb b/docs/examples/defiance_flight_sim.ipynb
index eb1479eb5..c8bbfa432 100644
--- a/docs/examples/defiance_flight_sim.ipynb
+++ b/docs/examples/defiance_flight_sim.ipynb
@@ -21,13 +21,13 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 1,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
     "import datetime\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket\n",
+    "from rocketpy import Environment, Flight, Function, HemisphericalParachute, Rocket\n",
     "from rocketpy.motors import CylindricalTank, Fluid, HybridMotor\n",
     "from rocketpy.motors.tank import MassFlowRateBasedTank"
    ]
@@ -185,7 +185,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 4,
+   "execution_count": null,
    "metadata": {},
    "outputs": [
     {
@@ -221,11 +221,15 @@
     "\n",
     "defiance.add_tail(top_radius=0.07, bottom_radius=0.064, length=0.0597, position=0.1)\n",
     "\n",
-    "defiance.add_parachute(name=\"main\", cd_s=2.2, trigger=305, sampling_rate=100, lag=0)\n",
+    "Main = HemisphericalParachute(\n",
+    "    name=\"main\", cd_s=2.2, trigger=305, sampling_rate=100, lag=0\n",
+    ")\n",
     "\n",
-    "defiance.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    name=\"drogue\", cd_s=1.55, trigger=\"apogee\", sampling_rate=100, lag=0\n",
-    ")"
+    ")\n",
+    "defiance.add_parachute(parachute=Main)\n",
+    "defiance.add_parachute(parachute=Drogue)"
    ]
   },
   {
diff --git a/docs/examples/genesis_flight_sim.ipynb b/docs/examples/genesis_flight_sim.ipynb
index cbda3ed6f..295387195 100644
--- a/docs/examples/genesis_flight_sim.ipynb
+++ b/docs/examples/genesis_flight_sim.ipynb
@@ -37,7 +37,7 @@
    "source": [
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket\n",
+    "from rocketpy import Environment, Flight, Function, HemisphericalParachute, Rocket\n",
     "from rocketpy.motors import SolidMotor\n",
     "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
@@ -267,11 +267,11 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 8,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Drogue = GENESIS.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    name=\"Drogue\",\n",
     "    cd_s=0.285005285533666,\n",
     "    trigger=\"apogee\",\n",
@@ -280,14 +280,16 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "Main = GENESIS.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    name=\"Main\",\n",
     "    cd_s=1.1,\n",
     "    trigger=870,\n",
     "    sampling_rate=105,\n",
     "    lag=1,\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "GENESIS.add_parachute(parachute=Drogue)\n",
+    "GENESIS.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/halcyon_flight_sim.ipynb b/docs/examples/halcyon_flight_sim.ipynb
index 503961448..ad10aa412 100644
--- a/docs/examples/halcyon_flight_sim.ipynb
+++ b/docs/examples/halcyon_flight_sim.ipynb
@@ -31,7 +31,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -39,7 +39,7 @@
     "\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket\n",
+    "from rocketpy import Environment, Flight, Function, HemisphericalParachute, Rocket\n",
     "from rocketpy.motors import CylindricalTank, Fluid, HybridMotor\n",
     "from rocketpy.motors.tank import MassFlowRateBasedTank\n",
     "\n",
@@ -416,17 +416,18 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 11,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Main = HALCYON.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    name=\"Main\",\n",
     "    cd_s=9.621,\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=100,\n",
     "    lag=5,\n",
-    ")"
+    ")\n",
+    "HALCYON.add_parachute(parachute=Main)"
    ]
   },
   {
diff --git a/docs/examples/index.rst b/docs/examples/index.rst
index e2919563f..6cc4356f4 100644
--- a/docs/examples/index.rst
+++ b/docs/examples/index.rst
@@ -32,6 +32,7 @@ apogee of some rockets.
       "Lince (2023)": (3284.12, 3587),
       "Defiance (2024)": (9238.01, 9308.32),
       "Hedy (2025)": (5406.92, 5231.53),
+      "Valkyrie (2025)": (2247.84, 2098.02),
    }
 
    max_apogee = 10000
@@ -104,5 +105,6 @@ In the next sections you will find the simulations of the rockets listed above.
    lince_flight_sim.ipynb
    defiance_flight_sim.ipynb
    hedy_flight_sim.ipynb
+   valkyrie_flight_sim.ipynb
 
 
diff --git a/docs/examples/juno3_flight_sim.ipynb b/docs/examples/juno3_flight_sim.ipynb
index c733e759d..788b7348f 100644
--- a/docs/examples/juno3_flight_sim.ipynb
+++ b/docs/examples/juno3_flight_sim.ipynb
@@ -33,13 +33,20 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")\n",
     "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
     "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
@@ -333,18 +340,19 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 15,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "drogue = juno.add_parachute(\n",
+    "drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=0.885,\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=105,\n",
     "    noise=(0, 8.3, 0.5),\n",
     "    lag=0.5,\n",
-    ")"
+    ")\n",
+    "juno.add_parachute(parachute=drogue)"
    ]
   },
   {
diff --git a/docs/examples/lince_flight_sim.ipynb b/docs/examples/lince_flight_sim.ipynb
index 39685bbf1..e2db12ba1 100644
--- a/docs/examples/lince_flight_sim.ipynb
+++ b/docs/examples/lince_flight_sim.ipynb
@@ -37,7 +37,14 @@
    "source": [
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")\n",
     "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
    ]
@@ -258,13 +265,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 7,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Main = LincePreDeploy.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
-    ")"
+    ")\n",
+    "LincePreDeploy.add_parachute(parachute=Main)"
    ]
   },
   {
@@ -321,13 +329,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 10,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Main_stage_1 = LincePostDeploy.add_parachute(\n",
+    "Main_stage_1 = HemisphericalParachute(\n",
     "    \"Main\", cd_s=3.9, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
-    ")"
+    ")\n",
+    "LincePostDeploy.add_parachute(parachute=Main_stage_1)"
    ]
   },
   {
@@ -389,13 +398,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 13,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "Main_stage_2 = Payload.add_parachute(\n",
+    "Main_stage_2 = HemisphericalParachute(\n",
     "    \"Main\", cd_s=0.159248, trigger=\"apogee\", sampling_rate=150, lag=0, noise=(0, 0, 0)\n",
-    ")"
+    ")\n",
+    "Payload.add_parachute(parachute=Main_stage_2)"
    ]
   },
   {
diff --git a/docs/examples/ndrt_2020_flight_sim.ipynb b/docs/examples/ndrt_2020_flight_sim.ipynb
index 2028824c9..84faa0831 100644
--- a/docs/examples/ndrt_2020_flight_sim.ipynb
+++ b/docs/examples/ndrt_2020_flight_sim.ipynb
@@ -29,7 +29,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -38,7 +38,14 @@
     "import numpy as np\n",
     "from scipy.signal import savgol_filter\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor"
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")"
    ]
   },
   {
@@ -367,11 +374,11 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 14,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "drogue = ndrt2020.add_parachute(\n",
+    "drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=parameters.get(\"cd_s_drogue\")[0],\n",
     "    trigger=\"apogee\",\n",
@@ -379,14 +386,17 @@
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
-    "main = ndrt2020.add_parachute(\n",
+    "main = HemisphericalParachute(\n",
     "    \"Main\",\n",
     "    cd_s=parameters.get(\"cd_s_main\")[0],\n",
     "    trigger=167.64,\n",
     "    sampling_rate=105,\n",
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "\n",
+    "ndrt2020.add_parachute(parachute=drogue)\n",
+    "ndrt2020.add_parachute(parachute=main)"
    ]
   },
   {
diff --git a/docs/examples/prometheus_2022_flight_sim.ipynb b/docs/examples/prometheus_2022_flight_sim.ipynb
index 9e4a157a2..22c53eba1 100644
--- a/docs/examples/prometheus_2022_flight_sim.ipynb
+++ b/docs/examples/prometheus_2022_flight_sim.ipynb
@@ -36,14 +36,21 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 3,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
     "import matplotlib.pyplot as plt\n",
     "import numpy as np\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, GenericMotor, Rocket\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    GenericMotor,\n",
+    "    HemisphericalParachute,\n",
+    "    Rocket,\n",
+    ")\n",
     "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
     "\n",
     "plt.style.use(\"seaborn-v0_8-colorblind\")"
@@ -217,7 +224,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 7,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -275,16 +282,19 @@
     "    position=0.273,\n",
     "    sweep_length=0.066,\n",
     ")\n",
-    "drogue = prometheus.add_parachute(\n",
+    "drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=1.6 * np.pi * 0.3048**2,  # Cd = 1.6, D_chute = 24 in\n",
     "    trigger=\"apogee\",\n",
     ")\n",
-    "main = prometheus.add_parachute(\n",
+    "main = HemisphericalParachute(\n",
     "    \"Main\",\n",
     "    cd_s=2.2 * np.pi * 0.9144**2,  # Cd = 2.2, D_chute = 72 in\n",
     "    trigger=457.2,  # 1500 ft\n",
-    ")"
+    ")\n",
+    "\n",
+    "prometheus.add_parachute(parachute=drogue)\n",
+    "prometheus.add_parachute(parachute=main)"
    ]
   },
   {
diff --git a/docs/examples/valetudo_flight_sim.ipynb b/docs/examples/valetudo_flight_sim.ipynb
index dd0a33c9c..53f53a89e 100644
--- a/docs/examples/valetudo_flight_sim.ipynb
+++ b/docs/examples/valetudo_flight_sim.ipynb
@@ -30,14 +30,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 31,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
     "# Importing libraries\n",
     "import matplotlib.pyplot as plt\n",
     "\n",
-    "from rocketpy import Environment, Flight, Rocket, SolidMotor"
+    "from rocketpy import Environment, Flight, HemisphericalParachute, Rocket, SolidMotor"
    ]
   },
   {
@@ -383,18 +383,19 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 40,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
-    "drogue = valetudo.add_parachute(\n",
+    "drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=parameters.get(\"cd_s_drogue\")[0],\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=105,\n",
     "    lag=parameters.get(\"lag_rec\")[0],\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "valetudo.add_parachute(parachute=drogue)"
    ]
   },
   {
diff --git a/docs/examples/valkyrie_flight_sim.ipynb b/docs/examples/valkyrie_flight_sim.ipynb
new file mode 100644
index 000000000..5bb47894e
--- /dev/null
+++ b/docs/examples/valkyrie_flight_sim.ipynb
@@ -0,0 +1,565 @@
+{
+ "cells": [
+  {
+   "cell_type": "markdown",
+   "id": "94a916eb",
+   "metadata": {},
+   "source": [
+    "# Valkyrie - Bisky Team - 2025\n",
+    "\n",
+    "Valkyrie has been an essential rocket to validate key technologies in recovery and avionics. It marked a significant step forward towards more efficient, precise, and safe rockets.\n",
+    "\n",
+    "Permission to use flight data given by Iñigo Martínez, 2026\n",
+    "\n",
+    "* Launch date: `July 26th, 2025`\n",
+    "\n",
+    "* Simulated Apogee: 2247.84 m\n",
+    "\n",
+    "* Recorded Apogee: 2098.02 m\n",
+    "\n",
+    "* Relative Error: `6.66%` "
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 71,
+   "id": "17ea162f",
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "%load_ext autoreload\n",
+    "%autoreload 2"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "id": "a4df1b07",
+   "metadata": {},
+   "source": [
+    "## Imports"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "id": "f0ed041a",
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "import json\n",
+    "\n",
+    "import matplotlib.pyplot as plt\n",
+    "\n",
+    "from rocketpy import Environment, Flight, Function, Rocket, SolidMotor\n",
+    "from rocketpy.simulation.flight_data_importer import FlightDataImporter\n",
+    "\n",
+    "plt.style.use(\"seaborn-v0_8-colorblind\")\n",
+    "\n",
+    "with open(\"../../data/rockets/valkyrie/VLK.json\", \"r\", encoding=\"utf-8\") as f:\n",
+    "    rocket_data = json.load(f)[\"VLK\"]\n",
+    "\n",
+    "with open(\"../../data/rockets/valkyrie/Dima.json\", \"r\", encoding=\"utf-8\") as f:\n",
+    "    launch_data = json.load(f)"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "id": "a8893b9b",
+   "metadata": {},
+   "source": [
+    "## Environment"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 7,
+   "id": "2be900a9",
+   "metadata": {},
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "\n",
+      "Gravity Details\n",
+      "\n",
+      "Acceleration of gravity at surface level:    9.8026 m/s²\n",
+      "Acceleration of gravity at   3.000 km (ASL): 9.7952 m/s²\n",
+      "\n",
+      "\n",
+      "Launch Site Details\n",
+      "\n",
+      "Launch Date: 2026-07-26 10:00:00 UTC | 2026-07-26 12:00:00 Europe/Madrid\n",
+      "Launch Site Latitude: 43.07777°\n",
+      "Launch Site Longitude: -2.68445°\n",
+      "Reference Datum: SIRGAS2000\n",
+      "Launch Site UTM coordinates: 37203.68 W    4785157.78 N\n",
+      "Launch Site UTM zone: 31T\n",
+      "Launch Site Surface Elevation: 605.0 m\n",
+      "\n",
+      "\n",
+      "Atmospheric Model Details\n",
+      "\n",
+      "Atmospheric Model Type: windy\n",
+      "windy Maximum Height: 3.000 km\n",
+      "\n",
+      "Surface Atmospheric Conditions\n",
+      "\n",
+      "Surface Wind Speed: 1.20 m/s\n",
+      "Surface Wind Direction: 129.36°\n",
+      "Surface Wind Heading: 309.36°\n",
+      "Surface Pressure: 946.36 hPa\n",
+      "Surface Temperature: 297.58 K\n",
+      "Surface Air Density: 1.108 kg/m³\n",
+      "Surface Speed of Sound: 345.82 m/s\n",
+      "\n",
+      "\n",
+      "Earth Model Details\n",
+      "\n",
+      "Earth Radius at Launch site: 6368.21 km\n",
+      "Semi-major Axis: 6378.14 km\n",
+      "Semi-minor Axis: 6356.75 km\n",
+      "Flattening: 0.0034\n",
+      "\n",
+      "\n",
+      "Atmospheric Model Plots\n",
+      "\n"
+     ]
+    },
+    {
+     "data": {
+      "image/png": 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",
+      "text/plain": [
+       "<Figure size 900x450 with 4 Axes>"
+      ]
+     },
+     "metadata": {},
+     "output_type": "display_data"
+    }
+   ],
+   "source": [
+    "env_cfg = launch_data[\"Environment\"]\n",
+    "\n",
+    "env = Environment(\n",
+    "    date=[2026, 7, 26, 12],\n",
+    "    latitude=env_cfg[\"latitude\"][\"value\"],\n",
+    "    longitude=env_cfg[\"longitude\"][\"value\"],\n",
+    "    elevation=env_cfg[\"elevation\"][\"value\"],\n",
+    "    timezone=env_cfg[\"timezone\"],\n",
+    ")\n",
+    "\n",
+    "env.set_atmospheric_model(type=\"windy\", file=\"ICON\")\n",
+    "env.max_expected_height = env_cfg[\"max_expected_height\"][\"value\"]\n",
+    "env.info()"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "id": "29b84c37",
+   "metadata": {},
+   "source": [
+    "## Motor"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 8,
+   "id": "95eb3add",
+   "metadata": {},
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "Nozzle Details\n",
+      "Nozzle Radius: 0.045 m\n",
+      "Nozzle Throat Radius: 0.023 m\n",
+      "\n",
+      "Grain Details\n",
+      "Number of Grains: 5\n",
+      "Grain Spacing: 0.001 m\n",
+      "Grain Density: 1170 kg/m3\n",
+      "Grain Outer Radius: 0.025 m\n",
+      "Grain Inner Radius: 0.01 m\n",
+      "Grain Height: 0.0966 m\n",
+      "Grain Volume: 0.000 m3\n",
+      "Grain Mass: 0.186 kg\n",
+      "\n",
+      "Motor Details\n",
+      "Total Burning Time: 3.5 s\n",
+      "Total Propellant Mass: 0.932 kg\n",
+      "Structural Mass Ratio: 0.409\n",
+      "Average Propellant Exhaust Velocity: 2142.979 m/s\n",
+      "Average Thrust: 570.679 N\n",
+      "Maximum Thrust: 1353.5 N at 0.011 s after ignition.\n",
+      "Total Impulse: 1997.377 Ns\n",
+      "\n"
+     ]
+    },
+    {
+     "name": "stderr",
+     "output_type": "stream",
+     "text": [
+      "c:\\Users\\emide\\anaconda3\\envs\\bisky_main\\Lib\\site-packages\\rocketpy\\motors\\motor.py:990: UserWarning: burn_time argument (0, 3.5) is out of thrust source time range. Using thrust_source boundary times instead: (0, 3.451) s.\n",
+      "If you want to change the burn out time of the curve please use the 'reshape_thrust_curve' argument.\n",
+      "  warnings.warn(\n"
+     ]
+    },
+    {
+     "data": {
+      "image/png": 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",
+      "text/plain": [
+       "<Figure size 640x480 with 1 Axes>"
+      ]
+     },
+     "metadata": {},
+     "output_type": "display_data"
+    }
+   ],
+   "source": [
+    "motor_cfg = rocket_data[\"motor\"]\n",
+    "\n",
+    "motor = SolidMotor(\n",
+    "    thrust_source=\"../../data/motors/cesaroni/Cesaroni_1997K650-21A.eng\",\n",
+    "    burn_time=motor_cfg[\"motor_burn_time\"][\"value\"],\n",
+    "    grain_number=int(motor_cfg[\"grain_number\"][\"value\"]),\n",
+    "    grain_density=motor_cfg[\"grain_density\"][\"value\"],\n",
+    "    grain_initial_inner_radius=motor_cfg[\"grain_initial_inner_radius\"][\"value\"],\n",
+    "    grain_outer_radius=motor_cfg[\"grain_outer_radius\"][\"value\"],\n",
+    "    grain_initial_height=motor_cfg[\"grain_initial_height\"][\"value\"],\n",
+    "    grain_separation=motor_cfg[\"grain_separation\"][\"value\"],\n",
+    "    grains_center_of_mass_position=motor_cfg[\"grains_center_of_mass_position\"][\"value\"],\n",
+    "    nozzle_radius=motor_cfg[\"nozzle_radius\"][\"value\"],\n",
+    "    throat_radius=motor_cfg[\"throat_radius\"][\"value\"],\n",
+    "    dry_mass=motor_cfg[\"motor_dry_mass\"][\"value\"],\n",
+    "    dry_inertia=(\n",
+    "        motor_cfg[\"motor_inertia_11\"][\"value\"],\n",
+    "        motor_cfg[\"motor_inertia_11\"][\"value\"],\n",
+    "        motor_cfg[\"motor_inertia_33\"][\"value\"],\n",
+    "    ),\n",
+    "    center_of_dry_mass_position=motor_cfg[\"motor_dry_mass_position\"][\"value\"],\n",
+    "    nozzle_position=motor_cfg[\"nozzle_position\"][\"value\"],\n",
+    "    coordinate_system_orientation=motor_cfg[\"motor_coordinate_system_orientation\"],\n",
+    ")\n",
+    "\n",
+    "motor.info()"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "id": "2e07459a",
+   "metadata": {},
+   "source": [
+    "## Rocket and Aerodynamic surfaces"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 9,
+   "id": "065222ad",
+   "metadata": {},
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "\n",
+      "Inertia Details\n",
+      "\n",
+      "Rocket Mass: 5.650 kg (without motor)\n",
+      "Rocket Dry Mass: 6.295 kg (with unloaded motor)\n",
+      "Rocket Loaded Mass: 7.227 kg\n",
+      "Rocket Structural Mass Ratio: 0.871\n",
+      "Rocket Inertia (with unloaded motor) 11: 2.047 kg*m2\n",
+      "Rocket Inertia (with unloaded motor) 22: 2.047 kg*m2\n",
+      "Rocket Inertia (with unloaded motor) 33: 0.019 kg*m2\n",
+      "Rocket Inertia (with unloaded motor) 12: 0.000 kg*m2\n",
+      "Rocket Inertia (with unloaded motor) 13: 0.000 kg*m2\n",
+      "Rocket Inertia (with unloaded motor) 23: 0.000 kg*m2\n",
+      "\n",
+      "Geometrical Parameters\n",
+      "\n",
+      "Rocket Maximum Radius: 0.055 m\n",
+      "Rocket Frontal Area: 0.009503 m2\n",
+      "\n",
+      "Rocket Distances\n",
+      "Rocket Center of Dry Mass - Center of Mass without Motor: 0.061 m\n",
+      "Rocket Center of Dry Mass - Nozzle Exit: 0.783 m\n",
+      "Rocket Center of Dry Mass - Center of Propellant Mass: 0.537 m\n",
+      "Rocket Center of Mass - Rocket Loaded Center of Mass: 0.069 m\n",
+      "\n",
+      "\n",
+      "Aerodynamics Lift Coefficient Derivatives\n",
+      "\n",
+      "Nose Cone Lift Coefficient Derivative: 2.000/rad\n",
+      "Fins Lift Coefficient Derivative: 4.927/rad\n",
+      "Tail Lift Coefficient Derivative: -1.405/rad\n",
+      "\n",
+      "Center of Pressure\n",
+      "\n",
+      "Nose Cone Center of Pressure position: 1.773 m\n",
+      "Fins Center of Pressure position: 0.061 m\n",
+      "Tail Center of Pressure position: -0.068 m\n",
+      "\n",
+      "Stability\n",
+      "\n",
+      "Center of Mass position (time=0): 0.714 m\n",
+      "Center of Pressure position (time=0): 0.714 m\n",
+      "Initial Static Margin (mach=0, time=0): -0.001 c\n",
+      "Final Static Margin (mach=0, time=burn_out): 0.628 c\n",
+      "Rocket Center of Mass (time=0) - Center of Pressure (mach=0): 0.000 m\n",
+      "\n",
+      "\n",
+      "Parachute Details\n",
+      "\n",
+      "Parachute Drogue with a cd_s of 0.2589 m2\n",
+      "Ejection signal trigger: At Apogee\n",
+      "Ejection system refresh rate: 105.000 Hz\n",
+      "Time between ejection signal is triggered and the parachute is fully opened: 1.7 s\n",
+      "\n",
+      "\n",
+      "Parachute Details\n",
+      "\n",
+      "Parachute Main with a cd_s of 5.7865 m2\n",
+      "Ejection signal trigger: main_trigger\n",
+      "Ejection system refresh rate: 105.000 Hz\n",
+      "Time between ejection signal is triggered and the parachute is fully opened: 1.7 s\n",
+      "\n"
+     ]
+    },
+    {
+     "data": {
+      "image/png": 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",
+      "text/plain": [
+       "<Figure size 800x600 with 1 Axes>"
+      ]
+     },
+     "metadata": {},
+     "output_type": "display_data"
+    }
+   ],
+   "source": [
+    "rocket_cfg = rocket_data[\"rocket\"]\n",
+    "nose_cfg = rocket_data[\"nose\"]\n",
+    "fins_cfg = rocket_data[\"fins\"]\n",
+    "tail_cfg = rocket_data[\"tail\"]\n",
+    "rail_cfg = rocket_data[\"rail_buttons\"]\n",
+    "\n",
+    "vlk = Rocket(\n",
+    "    radius=rocket_cfg[\"rocket_radius\"][\"value\"],\n",
+    "    mass=rocket_cfg[\"rocket_mass\"][\"value\"],\n",
+    "    inertia=(\n",
+    "        rocket_cfg[\"rocket_inertia_11\"][\"value\"],\n",
+    "        rocket_cfg[\"rocket_inertia_11\"][\"value\"],\n",
+    "        rocket_cfg[\"rocket_inertia_33\"][\"value\"],\n",
+    "    ),\n",
+    "    center_of_mass_without_motor=rocket_cfg[\"rocket_center_of_mass_without_motor\"][\n",
+    "        \"value\"\n",
+    "    ],\n",
+    "    power_off_drag=motor_cfg[\"power_off_drag\"][\"value\"],\n",
+    "    power_on_drag=motor_cfg[\"power_on_drag\"][\"value\"],\n",
+    "    coordinate_system_orientation=rocket_cfg[\"rocket_coordinate_system_orientation\"],\n",
+    ")\n",
+    "\n",
+    "vlk.set_rail_buttons(\n",
+    "    rail_cfg[\"upper_button_position\"][\"value\"],\n",
+    "    rail_cfg[\"lower_button_position\"][\"value\"],\n",
+    "    rail_cfg[\"rail_angular_position\"][\"value\"],\n",
+    ")\n",
+    "\n",
+    "vlk.add_motor(motor, position=rocket_cfg[\"motor_position\"][\"value\"])\n",
+    "\n",
+    "vlk.add_nose(\n",
+    "    length=nose_cfg[\"nose_length\"][\"value\"],\n",
+    "    kind=nose_cfg[\"nose_kind\"],\n",
+    "    position=nose_cfg[\"nose_position\"][\"value\"],\n",
+    ")\n",
+    "\n",
+    "vlk.add_trapezoidal_fins(\n",
+    "    n=int(fins_cfg[\"fin_n\"][\"value\"]),\n",
+    "    span=fins_cfg[\"fin_span\"][\"value\"],\n",
+    "    root_chord=fins_cfg[\"fin_root_chord\"][\"value\"],\n",
+    "    tip_chord=fins_cfg[\"fin_tip_chord\"][\"value\"],\n",
+    "    sweep_length=fins_cfg[\"fin_sweep_length\"][\"value\"],\n",
+    "    position=fins_cfg[\"fin_position\"][\"value\"],\n",
+    "    cant_angle=fins_cfg[\"fin_cant_angle\"][\"value\"],\n",
+    ")\n",
+    "\n",
+    "vlk.add_tail(\n",
+    "    top_radius=tail_cfg[\"top_radius\"][\"value\"],\n",
+    "    bottom_radius=tail_cfg[\"bottom_radius\"][\"value\"],\n",
+    "    length=tail_cfg[\"length\"][\"value\"],\n",
+    "    position=tail_cfg[\"position\"][\"value\"],\n",
+    ")\n",
+    "\n",
+    "main_cfg = rocket_data[\"main_chute\"]\n",
+    "drogue_cfg = rocket_data[\"drogue_chute\"]\n",
+    "\n",
+    "\n",
+    "def main_trigger(p, h, y):\n",
+    "    return y[5] < 0 and h < 500\n",
+    "\n",
+    "\n",
+    "vlk.add_parachute(\n",
+    "    name=\"Drogue\",\n",
+    "    cd_s=drogue_cfg[\"cd_s_drogue\"][\"value\"],\n",
+    "    sampling_rate=drogue_cfg[\"drogue_sampling_rate\"][\"value\"],\n",
+    "    lag=drogue_cfg[\"drogue_lag\"][\"value\"],\n",
+    "    trigger=\"apogee\",\n",
+    "    noise=tuple(drogue_cfg[\"drogue_noise\"]),\n",
+    ")\n",
+    "\n",
+    "vlk.add_parachute(\n",
+    "    name=\"Main\",\n",
+    "    cd_s=main_cfg[\"cd_s_main\"][\"value\"],\n",
+    "    sampling_rate=main_cfg[\"main_sampling_rate\"][\"value\"],\n",
+    "    lag=main_cfg[\"main_lag\"][\"value\"],\n",
+    "    trigger=main_trigger,\n",
+    "    noise=tuple(main_cfg[\"main_noise\"]),\n",
+    ")\n",
+    "\n",
+    "vlk.info()\n",
+    "vlk.draw()"
+   ]
+  },
+  {
+   "cell_type": "markdown",
+   "id": "87c67151",
+   "metadata": {},
+   "source": [
+    "## Flight Simulation Data"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 10,
+   "id": "6dd42298",
+   "metadata": {},
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "\n",
+      "Apogee State\n",
+      "\n",
+      "Apogee Time: 20.884 s\n",
+      "Apogee Altitude: 2852.849 m (ASL) | 2247.849 m (AGL)\n",
+      "Apogee Freestream Speed: 6.868 m/s\n",
+      "Apogee X position: 148.646 m\n",
+      "Apogee Y position: 170.475 m\n",
+      "Apogee latitude: 43.0793048°\n",
+      "Apogee longitude: -2.6826150°\n"
+     ]
+    }
+   ],
+   "source": [
+    "flight_cfg = launch_data[\"Flight\"]\n",
+    "launch_cfg = launch_data[\"launch\"]\n",
+    "\n",
+    "flight = Flight(\n",
+    "    rocket=vlk,\n",
+    "    environment=env,\n",
+    "    rail_length=5,\n",
+    "    inclination=87,\n",
+    "    heading=30,\n",
+    "    max_time=2000,\n",
+    ")\n",
+    "\n",
+    "flight.prints.apogee_conditions()"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 11,
+   "id": "bfd25766",
+   "metadata": {},
+   "outputs": [
+    {
+     "data": {
+      "image/png": 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",
+      "text/plain": [
+       "<Figure size 900x900 with 1 Axes>"
+      ]
+     },
+     "metadata": {},
+     "output_type": "display_data"
+    }
+   ],
+   "source": [
+    "flight.plots.trajectory_3d()"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": 12,
+   "id": "aa85c425",
+   "metadata": {},
+   "outputs": [
+    {
+     "name": "stdout",
+     "output_type": "stream",
+     "text": [
+      "The following attributes were create and are now available to be used:  ['time', 'altitude']\n"
+     ]
+    },
+    {
+     "data": {
+      "image/png": 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",
+      "text/plain": [
+       "<Figure size 640x480 with 1 Axes>"
+      ]
+     },
+     "metadata": {},
+     "output_type": "display_data"
+    }
+   ],
+   "source": [
+    "columns_map = {\"time\": \"time\", \"altitude\": \"altitude\"}\n",
+    "\n",
+    "cots_altimeter_flight = FlightDataImporter(\n",
+    "    name=\"Altimeter Data\",\n",
+    "    paths=\"../../data/rockets/valkyrie/flightInfo_merged.csv\",\n",
+    "    columns_map=columns_map,\n",
+    "    units=None,\n",
+    "    interpolation=\"linear\",\n",
+    "    extrapolation=\"zero\",\n",
+    "    delimiter=\",\",\n",
+    "    encoding=\"utf-8\",\n",
+    ")\n",
+    "Function.compare_plots(\n",
+    "    [\n",
+    "        (flight.altitude, \"RocketPy\"),\n",
+    "        (cots_altimeter_flight.altitude, \"Altimeter\"),\n",
+    "    ],\n",
+    "    title=\"Altitude Comparison\",\n",
+    "    xlabel=\"Time (s)\",\n",
+    "    ylabel=\"Altitude (m)\",\n",
+    "    lower=0,\n",
+    "    upper=40,\n",
+    ")"
+   ]
+  }
+ ],
+ "metadata": {
+  "kernelspec": {
+   "display_name": "bisky_main",
+   "language": "python",
+   "name": "python3"
+  },
+  "language_info": {
+   "codemirror_mode": {
+    "name": "ipython",
+    "version": 3
+   },
+   "file_extension": ".py",
+   "mimetype": "text/x-python",
+   "name": "python",
+   "nbconvert_exporter": "python",
+   "pygments_lexer": "ipython3",
+   "version": "3.11.14"
+  }
+ },
+ "nbformat": 4,
+ "nbformat_minor": 5
+}
diff --git a/docs/notebooks/getting_started.ipynb b/docs/notebooks/getting_started.ipynb
index a5adf46d2..66d5e0b8a 100644
--- a/docs/notebooks/getting_started.ipynb
+++ b/docs/notebooks/getting_started.ipynb
@@ -42,7 +42,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": null,
    "metadata": {
     "colab": {},
     "colab_type": "code",
@@ -50,7 +50,7 @@
    },
    "outputs": [],
    "source": [
-    "from rocketpy import Environment, Flight, Rocket, SolidMotor"
+    "from rocketpy import Environment, Flight, HemisphericalParachute, Rocket, SolidMotor"
    ]
   },
   {
@@ -721,7 +721,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 14,
+   "execution_count": null,
    "metadata": {
     "colab": {},
     "colab_type": "code",
@@ -729,7 +729,7 @@
    },
    "outputs": [],
    "source": [
-    "Main = calisto.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    \"Main\",\n",
     "    cd_s=10.0,\n",
     "    trigger=800,\n",
@@ -738,14 +738,17 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "Drogue = calisto.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=1.0,\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=105,\n",
     "    lag=1.5,\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "\n",
+    "calisto.add_parachute(parachute=Main)\n",
+    "calisto.add_parachute(parachute=Drogue)"
    ]
   },
   {
@@ -1246,24 +1249,10 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 17,
+   "execution_count": null,
    "metadata": {},
-   "outputs": [
-    {
-     "name": "stdout",
-     "output_type": "stream",
-     "text": [
-      "File  trajectory.kml  saved with success!\n"
-     ]
-    }
-   ],
-   "source": [
-    "test_flight.export_kml(\n",
-    "    file_name=\"trajectory.kml\",\n",
-    "    extrude=True,\n",
-    "    altitude_mode=\"relative_to_ground\",\n",
-    ")"
-   ]
+   "outputs": [],
+   "source": "from rocketpy.simulation import FlightDataExporter\n\nFlightDataExporter(test_flight).export_kml(\n    file_name=\"trajectory.kml\",\n    extrude=True,\n    altitude_mode=\"relative_to_ground\",\n)"
   },
   {
    "attachments": {},
@@ -1568,6 +1557,9 @@
   }
  ],
  "metadata": {
+  "nbsphinx": {
+   "orphan": true
+  },
   "colab": {
    "name": "getting_started.ipynb",
    "provenance": [],
@@ -1575,7 +1567,7 @@
   },
   "hide_input": false,
   "kernelspec": {
-   "display_name": ".venv12",
+   "display_name": "rocketpy_dev_venv (3.12.3)",
    "language": "python",
    "name": "python3"
   },
@@ -1589,9 +1581,9 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.12.4"
+   "version": "3.12.3"
   }
  },
  "nbformat": 4,
  "nbformat_minor": 2
-}
+}
\ No newline at end of file
diff --git a/docs/notebooks/getting_started_colab.ipynb b/docs/notebooks/getting_started_colab.ipynb
index ef0f7e711..783c72a3a 100644
--- a/docs/notebooks/getting_started_colab.ipynb
+++ b/docs/notebooks/getting_started_colab.ipynb
@@ -67,7 +67,7 @@
    },
    "outputs": [],
    "source": [
-    "from rocketpy import Environment, Flight, Rocket, SolidMotor"
+    "from rocketpy import Environment, Flight, HemisphericalParachute, Rocket, SolidMotor"
    ]
   },
   {
@@ -485,7 +485,7 @@
    },
    "outputs": [],
    "source": [
-    "Main = calisto.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    \"Main\",\n",
     "    cd_s=10.0,\n",
     "    trigger=800,\n",
@@ -494,14 +494,17 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "Drogue = calisto.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=1.0,\n",
     "    trigger=\"apogee\",\n",
     "    sampling_rate=105,\n",
     "    lag=1.5,\n",
     "    noise=(0, 8.3, 0.5),\n",
-    ")"
+    ")\n",
+    "\n",
+    "calisto.add_parachute(parachute=Main)\n",
+    "calisto.add_parachute(parachute=Drogue)"
    ]
   },
   {
@@ -588,13 +591,19 @@
    "execution_count": null,
    "metadata": {},
    "outputs": [],
-   "source": [
-    "test_flight.export_kml(\n",
-    "    file_name=\"trajectory.kml\",\n",
-    "    extrude=True,\n",
-    "    altitude_mode=\"relative_to_ground\",\n",
-    ")"
-   ]
+   "source": "from rocketpy.simulation import FlightDataExporter\n\nFlightDataExporter(test_flight).export_kml(\n    file_name=\"trajectory.kml\",\n    extrude=True,\n    altitude_mode=\"relative_to_ground\",\n)"
+  },
+  {
+   "cell_type": "markdown",
+   "source": "## 3D Flight Animation\n\nRocketPy can render an interactive 3D animation of the rocket's trajectory and attitude using [vedo](https://vedo.embl.es/). This feature requires the optional `animation` extra:\n\n```bash\npip install rocketpy[animation]\n```\n\n> **Note:** The interactive animation window opens in a desktop environment. It will not display inside Google Colab or other headless notebook servers — run it locally for the best experience.\n\nTwo animation modes are available:\n\n| Method | What it shows |\n|---|---|\n| `flight.plots.animate_trajectory()` | Rocket moves through 3D space following the simulated trajectory |\n| `flight.plots.animate_rotate()` | Rocket stays centred; only attitude (rotation) is animated |\n\nBoth methods accept an optional `file_name` argument pointing to a custom `.stl` model. When omitted, RocketPy uses a built-in default rocket shape.",
+   "metadata": {}
+  },
+  {
+   "cell_type": "code",
+   "source": "# Install the optional animation dependency (skip if already installed)\n!pip install \"rocketpy[animation]\"\n\n# Animate the full trajectory — rocket moves through 3D space\n# Press Escape or close the window to exit the animation\ntest_flight.plots.animate_trajectory(\n    start=0,\n    stop=test_flight.t_final,\n    time_step=0.05,\n)\n\n# Alternatively, animate only the attitude changes (rocket stays centred)\n# test_flight.plots.animate_rotate(\n#     start=0,\n#     stop=test_flight.t_final,\n#     time_step=0.05,\n# )\n\n# To use your own 3D model, pass its path via file_name:\n# test_flight.plots.animate_trajectory(file_name=\"my_rocket.stl\")",
+   "metadata": {},
+   "execution_count": null,
+   "outputs": []
   },
   {
    "attachments": {},
@@ -798,6 +807,9 @@
   }
  ],
  "metadata": {
+  "nbsphinx": {
+   "orphan": true
+  },
   "colab": {
    "name": "getting_started.ipynb",
    "provenance": [],
@@ -824,4 +836,4 @@
  },
  "nbformat": 4,
  "nbformat_minor": 2
-}
+}
\ No newline at end of file
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis.ipynb b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis.ipynb
index 581266045..617a59be5 100644
--- a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis.ipynb
+++ b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis.ipynb
@@ -80,7 +80,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 1,
+   "execution_count": null,
    "metadata": {
     "id": "rNY7u8fApOP_"
    },
@@ -92,7 +92,7 @@
     "from IPython.display import display\n",
     "from numpy.random import choice, normal\n",
     "\n",
-    "from rocketpy import Environment, Flight, Rocket, SolidMotor"
+    "from rocketpy import Environment, Flight, HemisphericalParachute, Rocket, SolidMotor"
    ]
   },
   {
@@ -369,7 +369,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 6,
+   "execution_count": null,
    "metadata": {
     "colab": {
      "base_uri": "https://localhost:8080/",
@@ -495,7 +495,7 @@
     "        airfoil=None,\n",
     "    )\n",
     "    # Add parachute\n",
-    "    Drogue = Valetudo.add_parachute(\n",
+    "    Drogue = HemisphericalParachute(\n",
     "        \"Drogue\",\n",
     "        cd_s=setting[\"cd_s_drogue\"],\n",
     "        trigger=drogue_trigger,\n",
@@ -503,6 +503,7 @@
     "        lag=setting[\"lag_rec\"] + setting[\"lag_se\"],\n",
     "        noise=(0, 8.3, 0.5),\n",
     "    )\n",
+    "    Valetudo.add_parachute(parachute=Drogue)\n",
     "\n",
     "    # Run trajectory simulation\n",
     "    try:\n",
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb b/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb
index 2fb46fa86..11e5b6487 100644
--- a/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb
+++ b/docs/notebooks/monte_carlo_analysis/monte_carlo_class_usage.ipynb
@@ -47,13 +47,21 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
     "import datetime\n",
     "\n",
-    "from rocketpy import Environment, Flight, Function, MonteCarlo, Rocket, SolidMotor\n",
+    "from rocketpy import (\n",
+    "    Environment,\n",
+    "    Flight,\n",
+    "    Function,\n",
+    "    HemisphericalParachute,\n",
+    "    MonteCarlo,\n",
+    "    Rocket,\n",
+    "    SolidMotor,\n",
+    ")\n",
     "from rocketpy.stochastic import (\n",
     "    StochasticEnvironment,\n",
     "    StochasticFlight,\n",
@@ -107,7 +115,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 4,
+   "execution_count": null,
    "metadata": {},
    "outputs": [
     {
@@ -180,7 +188,7 @@
     "tail = rocket.add_tail(\n",
     "    top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656\n",
     ")\n",
-    "Main = rocket.add_parachute(\n",
+    "Main = HemisphericalParachute(\n",
     "    \"Main\",\n",
     "    cd_s=10.0,\n",
     "    trigger=800,\n",
@@ -189,7 +197,7 @@
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
     "\n",
-    "Drogue = rocket.add_parachute(\n",
+    "Drogue = HemisphericalParachute(\n",
     "    \"Drogue\",\n",
     "    cd_s=1.0,\n",
     "    trigger=\"apogee\",\n",
@@ -197,6 +205,8 @@
     "    lag=1.5,\n",
     "    noise=(0, 8.3, 0.5),\n",
     ")\n",
+    "rocket.add_parachute(parachute=Main)\n",
+    "rocket.add_parachute(parachute=Drogue)\n",
     "\n",
     "# Flight\n",
     "test_flight = Flight(\n",
@@ -601,7 +611,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 13,
+   "execution_count": null,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -612,8 +622,8 @@
     "stochastic_rocket.set_rail_buttons(\n",
     "    stochastic_rail_buttons, lower_button_position=(0.001, \"normal\")\n",
     ")\n",
-    "stochastic_rocket.add_parachute(stochastic_main)\n",
-    "stochastic_rocket.add_parachute(stochastic_drogue)"
+    "stochastic_rocket.add_parachute(parachute=stochastic_main)\n",
+    "stochastic_rocket.add_parachute(parachute=stochastic_drogue)"
    ]
   },
   {
@@ -800,6 +810,28 @@
     ")"
    ]
   },
+  {
+   "cell_type": "markdown",
+   "metadata": {},
+   "source": [
+    "Alternatively, we can target an attribute using the method `MonteCarlo.simulate_convergence()` such that when the tolerance is met, the flight simulations would terminate early."
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "test_dispersion.simulate_convergence(\n",
+    "    target_attribute=\"apogee_time\",\n",
+    "    target_confidence=0.95,\n",
+    "    tolerance=0.5,  # in seconds\n",
+    "    max_simulations=1000,\n",
+    "    batch_size=50,\n",
+    ")"
+   ]
+  },
   {
    "attachments": {},
    "cell_type": "markdown",
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_sensitivity_simulation.py b/docs/notebooks/monte_carlo_analysis/monte_carlo_sensitivity_simulation.py
index fc471ffad..4c965bd19 100644
--- a/docs/notebooks/monte_carlo_analysis/monte_carlo_sensitivity_simulation.py
+++ b/docs/notebooks/monte_carlo_analysis/monte_carlo_sensitivity_simulation.py
@@ -11,7 +11,14 @@
 import datetime
 
 # %%
-from rocketpy import Environment, Flight, MonteCarlo, Rocket, SolidMotor
+from rocketpy import (
+    Environment,
+    Flight,
+    HemisphericalParachute,
+    MonteCarlo,
+    Rocket,
+    SolidMotor,
+)
 from rocketpy.stochastic import (
     StochasticEnvironment,
     StochasticFlight,
@@ -135,7 +142,7 @@
 tail = rocket.add_tail(
     top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656
 )
-Main = rocket.add_parachute(
+Main = HemisphericalParachute(
     "Main",
     cd_s=analysis_parameters["parachutes_main_cd_s"]["mean"],
     lag=analysis_parameters["parachutes_main_lag"]["mean"],
@@ -144,7 +151,7 @@
     noise=(0, 8.3, 0.5),
 )
 
-Drogue = rocket.add_parachute(
+Drogue = HemisphericalParachute(
     "Drogue",
     cd_s=analysis_parameters["parachutes_drogue_cd_s"]["mean"],
     lag=analysis_parameters["parachutes_drogue_lag"]["mean"],
@@ -153,6 +160,9 @@
     noise=(0, 8.3, 0.5),
 )
 
+rocket.add_parachute(parachute=Main)
+rocket.add_parachute(parachute=Drogue)
+
 # Flight
 test_flight = Flight(
     rocket=rocket,
diff --git a/docs/reference/classes/Parachute.rst b/docs/reference/classes/Parachute.rst
index f2ffb983d..88dd938e2 100644
--- a/docs/reference/classes/Parachute.rst
+++ b/docs/reference/classes/Parachute.rst
@@ -2,4 +2,10 @@ Parachute Class
 ---------------
 
 .. autoclass:: rocketpy.Parachute
+   :members:
+
+HemisphericalParachute Class
+----------------------------
+
+.. autoclass:: rocketpy.HemisphericalParachute
    :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/EllipticalFin.rst b/docs/reference/classes/aero_surfaces/EllipticalFin.rst
new file mode 100644
index 000000000..3f1403e8e
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/EllipticalFin.rst
@@ -0,0 +1,5 @@
+EllipticalFin Class
+-------------------
+
+.. autoclass:: rocketpy.EllipticalFin
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/Fin.rst b/docs/reference/classes/aero_surfaces/Fin.rst
new file mode 100644
index 000000000..b9c70c25e
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/Fin.rst
@@ -0,0 +1,5 @@
+Fin Class
+---------
+
+.. autoclass:: rocketpy.Fin
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/FreeFormFin.rst b/docs/reference/classes/aero_surfaces/FreeFormFin.rst
new file mode 100644
index 000000000..636be2c9e
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/FreeFormFin.rst
@@ -0,0 +1,5 @@
+FreeFormFin Class
+-----------------
+
+.. autoclass:: rocketpy.FreeFormFin
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/FreeFormFins.rst b/docs/reference/classes/aero_surfaces/FreeFormFins.rst
new file mode 100644
index 000000000..c641ce156
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/FreeFormFins.rst
@@ -0,0 +1,5 @@
+FreeFormFins Class
+------------------
+
+.. autoclass:: rocketpy.FreeFormFins
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/TrapezoidalFin.rst b/docs/reference/classes/aero_surfaces/TrapezoidalFin.rst
new file mode 100644
index 000000000..34fa631df
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/TrapezoidalFin.rst
@@ -0,0 +1,5 @@
+TrapezoidalFin Class
+--------------------
+
+.. autoclass:: rocketpy.TrapezoidalFin
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/_BaseFin.rst b/docs/reference/classes/aero_surfaces/_BaseFin.rst
new file mode 100644
index 000000000..358668e1f
--- /dev/null
+++ b/docs/reference/classes/aero_surfaces/_BaseFin.rst
@@ -0,0 +1,7 @@
+:orphan:
+
+_BaseFin Class
+--------------
+
+.. autoclass:: rocketpy.rocket.aero_surface.fins._base_fin._BaseFin
+   :members:
\ No newline at end of file
diff --git a/docs/reference/classes/aero_surfaces/index.rst b/docs/reference/classes/aero_surfaces/index.rst
index c6e6a3efe..a3dad0417 100644
--- a/docs/reference/classes/aero_surfaces/index.rst
+++ b/docs/reference/classes/aero_surfaces/index.rst
@@ -11,7 +11,12 @@ AeroSurface Classes
    Fins
    TrapezoidalFins
    EllipticalFins
+   FreeFormFins
+   Fin
+   TrapezoidalFin
+   EllipticalFin
+   FreeFormFin
    RailButtons
    AirBrakes
    GenericSurface
-   LinearGenericSurface
+   LinearGenericSurface
\ No newline at end of file
diff --git a/docs/reference/classes/exceptions.rst b/docs/reference/classes/exceptions.rst
new file mode 100644
index 000000000..f1dfe24b6
--- /dev/null
+++ b/docs/reference/classes/exceptions.rst
@@ -0,0 +1,14 @@
+Exceptions and Warnings
+=======================
+
+RocketPy raises a small hierarchy of custom exceptions and warnings so that
+error handling can be more specific than catching plain ``ValueError`` or
+``UserWarning``. All exceptions inherit from :class:`~rocketpy.exceptions.RocketPyError`,
+which makes it possible to catch any RocketPy-specific error with a single
+``except`` clause while still deriving from the relevant built-in type
+(e.g. :class:`~rocketpy.exceptions.InvalidParameterError` is also a
+``ValueError``).
+
+.. automodule:: rocketpy.exceptions
+   :members:
+   :show-inheritance:
diff --git a/docs/reference/classes/motors/RingClusterMotor.rst b/docs/reference/classes/motors/RingClusterMotor.rst
new file mode 100644
index 000000000..5178216e1
--- /dev/null
+++ b/docs/reference/classes/motors/RingClusterMotor.rst
@@ -0,0 +1,5 @@
+RingClusterMotor Class
+----------------------
+
+.. autoclass:: rocketpy.RingClusterMotor
+   :members:
diff --git a/docs/reference/classes/motors/index.rst b/docs/reference/classes/motors/index.rst
index 3bd6e2d96..b98748afd 100644
--- a/docs/reference/classes/motors/index.rst
+++ b/docs/reference/classes/motors/index.rst
@@ -10,6 +10,7 @@ Motor Classes
    HybridMotor
    LiquidMotor
    GenericMotor
+   RingClusterMotor
    Fluid
    Tank Classes <tanks/index>
    Tank Geometry Classes <geometries/index>
diff --git a/docs/reference/classes/utils/index.rst b/docs/reference/classes/utils/index.rst
index 05fffd9e9..150f78d03 100644
--- a/docs/reference/classes/utils/index.rst
+++ b/docs/reference/classes/utils/index.rst
@@ -7,7 +7,8 @@ Utils functions
 
    tools
    units
-   utilities   
+   utilities
    vector
    matrix
-   
+   logging
+
diff --git a/docs/reference/classes/utils/logging.rst b/docs/reference/classes/utils/logging.rst
new file mode 100644
index 000000000..c2e933a76
--- /dev/null
+++ b/docs/reference/classes/utils/logging.rst
@@ -0,0 +1,4 @@
+Logging functions
+-----------------
+
+.. autofunction:: rocketpy.utilities.enable_logging
diff --git a/docs/reference/classes/utils/utilities.rst b/docs/reference/classes/utils/utilities.rst
index 6376c2aad..b4bde76ca 100644
--- a/docs/reference/classes/utils/utilities.rst
+++ b/docs/reference/classes/utils/utilities.rst
@@ -11,4 +11,5 @@ At RocketPy projects, utilities are functions that:
 Below you have a list of all utilities functions available in rocketpy. 
 
 .. automodule:: rocketpy.utilities
-   :members:
\ No newline at end of file
+   :members:
+   :exclude-members: enable_logging
\ No newline at end of file
diff --git a/docs/reference/index.rst b/docs/reference/index.rst
index de3b36ac8..48d54d989 100644
--- a/docs/reference/index.rst
+++ b/docs/reference/index.rst
@@ -18,9 +18,10 @@ This reference manual details functions, modules, methods and attributes include
    classes/Flight
    Utilities <classes/utils/index>
    classes/EnvironmentAnalysis
-   Monte Carlo Analysis <classes/monte_carlo/index> 
+   Monte Carlo Analysis <classes/monte_carlo/index>
    Sensitivity Analysis <classes/Sensitivity>
    Multivariate Rejection Sampler <classes/MultivariateRejectionSampler>
+   Exceptions and Warnings <classes/exceptions>
 
 .. toctree::
    :maxdepth: 2
diff --git a/docs/static/rocket/fin_forces.png b/docs/static/rocket/fin_forces.png
new file mode 100644
index 000000000..41be9bfa2
Binary files /dev/null and b/docs/static/rocket/fin_forces.png differ
diff --git a/docs/static/rocket/individual_fin_frame.png b/docs/static/rocket/individual_fin_frame.png
new file mode 100644
index 000000000..67d417cdb
Binary files /dev/null and b/docs/static/rocket/individual_fin_frame.png differ
diff --git a/docs/technical/aerodynamics/individual_fins.rst b/docs/technical/aerodynamics/individual_fins.rst
new file mode 100644
index 000000000..408352e16
--- /dev/null
+++ b/docs/technical/aerodynamics/individual_fins.rst
@@ -0,0 +1,498 @@
+.. _individual_fins:
+
+====================
+Individual Fin Model
+====================
+
+:Author: Mateus Stano Junqueira
+:Date: March 2025
+
+Introduction
+============
+
+There are currently three ways to model the aerodynamic effects of fins in RocketPy:
+
+1. By use of the :class:`rocketpy.GenericSurface` or :class:`rocketpy.LinearGenericSurface` classes,
+   which are defined by receiving the aerodynamic coefficients directly;
+2. By use of the :class:`rocketpy.Fins` classes (:class:`rocketpy.TrapezoidalFins`, :class:`rocketpy.EllipticalFins`, :class:`rocketpy.FreeFormFins`),
+   which are defined by receiving the geometric parameters of the **fin set** and 
+   calculating the aerodynamic coefficients internally with the Barrowman method;
+3. By use of the :class:`rocketpy.Fin` classes (:class:`rocketpy.TrapezoidalFin`, :class:`rocketpy.EllipticalFin`, :class:`rocketpy.FreeFormFin`)
+   (which are the base classes for the fin set classes), which are defined by receiving the 
+   geometric parameters of **one single fin** and calculating the aerodynamic
+   coefficients internally with the Barrowman method, with exception of the
+   moment coefficients, which have been derived in this document.
+
+This document will focus on all the mathematical derivations and implementations
+of the :class:`rocketpy.Fin` classes.
+
+Fin Coordinate Frame
+====================
+
+The fin coordinate frame is defined as follows:
+
+- The origin is at the leading edge of the fin, at the intersection of the
+  fin's root chord and the fin's leading edge;
+- The z-axis is aligned with the fin's root chord, pointing towards the fin's
+  trailing edge;
+- The y-axis is aligned with the fin's span, pointing towards the fin's tip chord;
+- The x-axis completes the right-handed coordinate system.
+
+The fin is postioned at the rocket's body, given a ``rocket_radius`` :math:`r`, 
+an  ``angular_position`` :math:`\Gamma` and a position :math:`p` along the 
+rocket's body. The angular position is given according to 
+:ref:`Angular Position Inputs <angular_position>`.
+
+
+The fin can also be rotated by a cant angle :math:`\delta`.
+
+The image below shows the fin coordinate frame:
+
+.. image:: ../../static/rocket/individual_fin_frame.png
+   :width: 800
+   :align: center
+
+.. note::
+  A positive cant angle :math:`\delta` produces a negative body axis rolling 
+  moment at zero angle of attack.
+
+The rotation matrix from the fin coordinate frame to the rocket's body frame is
+define by, first a rotation around the y-axis by 180 degrees:
+
+.. math::
+  \mathbf{R}_{y(\pi)} = \begin{bmatrix}
+    -1 & 0 & 0 \\
+    0 & 1 & 0 \\
+    0 & 0 & -1
+  \end{bmatrix}
+
+Then a rotation around the z-axis by the angle :math:`\Gamma`:
+
+.. math::
+  \mathbf{R}_{z(\Gamma)} = \begin{bmatrix}
+    \cos(\Gamma) & -\sin(\Gamma) & 0 \\
+    \sin(\Gamma) & \cos(\Gamma) & 0 \\
+    0 & 0 & 1
+  \end{bmatrix}
+
+Then a rotation around the y-axis by the cant angle :math:`\delta`:
+
+.. math::
+  \mathbf{R}_{y(\delta)} = \begin{bmatrix}
+    \cos(\delta) & 0 & \sin(\delta) \\
+    0 & 1 & 0 \\
+    -\sin(\delta) & 0 & \cos(\delta)
+  \end{bmatrix}
+
+The final rotation matrix is given by:
+
+.. math::
+  \mathbf{R} = \mathbf{R}_{y(\delta)} \cdot \mathbf{R}_{z(\Gamma)} \cdot \mathbf{R}_{y(\pi)}
+
+
+The position of the fin's coordinate frame origin in the rocket's body frame
+is calculated by first assuming no a fin frame with no cant angle, then
+calculating the position of the fin's leading edge (with cant angle) in this 
+frame, and finally translating this position to the fin's position in the
+rocket's body frame. The position of the fin's real leading edge in this no cant 
+angle fin frame is given by the point :math:`\mathbf{P}^{\delta}_{le_f}`:
+
+.. math::
+  \mathbf{P}^{\delta}_{le_f} = \begin{bmatrix}
+    -\frac{Cr}{2} \sin(\delta) \\
+    0 \\
+    \frac{Cr}{2} (1 - \cos(\delta))
+  \end{bmatrix}
+
+Then, describing this point to the rocket's body frame orientation (no 
+translation):
+
+.. math::
+  \mathbf{P}^{\delta}_{le_b} = (\mathbf{R}_{z(\Gamma)} \cdot \mathbf{R}_{y(\pi)}) \cdot \mathbf{P}^{\delta}_{le_f}
+
+The position of the fin's leading edge with no cant angle in the rocket's body
+frame is given by:
+
+.. math::
+  \mathbf{P}^{\overline{\delta}}_{le_b} = \begin{bmatrix}
+    -r \sin(\Gamma) \\
+    r \cos(\Gamma) \\
+    p
+  \end{bmatrix}
+
+Finally, we add the position of the fin's leading edge with no cant angle to the
+position of the fin's leading edge with cant angle in the rocket's body frame:
+
+.. math::
+  \mathbf{P}_{le_b} = \mathbf{P}^{\overline{\delta}}_{le_b} + \mathbf{P}^{\delta}_{le_b}
+
+
+Center of Pressure Position
+===========================
+
+In the Fin Coordinate Frame, the center of pressure is given by the Barrowman
+method, and will here only be defined symbolically:
+
+.. math::
+  \mathbf{cp}_f = \begin{bmatrix}
+    cp_x \\
+    cp_y \\
+    cp_z
+  \end{bmatrix}
+
+The center of pressure position in the rocket's body frame is given by:
+
+.. math::
+  \mathbf{cp}_{rocket} = \mathbf{R} \cdot \mathbf{cp}_f + \mathbf{P}_{le_b}
+
+Aerodynamic Forces
+==================
+
+.. note::
+  The aerodynamic coefficients are defined according the Barrowman method.
+
+Given a stream velocity in the fin frame :math:`\mathbf{v}_{0f} = [v_{0x}, v_{0y}, v_{0z}]^{T}`,
+the effective angle of attack of the fin is given by:
+
+.. math::
+  \alpha_f = \arctan\left(\frac{v_{0x}}{v_{0z}}\right)
+
+This can also be seen as the angle between the fin's root chord and the stream
+velocity vector in the fin frame.
+
+The aerodynamic force in the x-direction of the fin is given by:
+
+.. math::
+  F_{x} = \frac{1}{2} \cdot \rho \cdot \|\mathbf{v}_{0f}\|^2 \cdot A_{r} \cdot C_{N}(\alpha_f, Ma)
+
+Where :math:`A_{r}` is the reference area of the fin, and :math:`C_{N}` is the
+normal force coefficient, which is a function of the angle of attack and the
+Mach number :math:`Ma`.
+This force is then transformed to the rocket's body frame by the rotation matrix:
+
+.. math::
+  \begin{bmatrix}
+    F_{x} \\
+    F_{y} \\
+    F_{z}
+  \end{bmatrix}_{rocket} = \mathbf{R} \cdot \begin{bmatrix}
+    F_{x} \\
+    0 \\
+    0
+  \end{bmatrix}_{fin}
+
+Then, the moments are calculated by the cross product of the center of pressure
+and the aerodynamic force:
+
+.. math::
+  \begin{bmatrix}
+    M_{x} \\
+    M_{y} \\
+    M_{z}
+  \end{bmatrix}_{rocket} = \mathbf{cp}_{rocket} \times \begin{bmatrix}
+    F_{x} \\
+    F_{y} \\
+    F_{z}
+  \end{bmatrix}_{rocket}
+
+From the Barrowman method, the moment along the center axis of the rocket
+(:math:`M_{z}`) is still missing the damping term, which is given by:
+
+.. math::
+  M_{damp} = \frac{1}{2} \cdot \rho \cdot \|v_{0}\| \cdot A_{r} \cdot L_{r}^2 \cdot C_{ld\omega}(Ma) \cdot \frac{1}{2} \cdot \omega_z 
+
+.. math::
+  M_{z \, \text{final}} = M_{z} + M_{damp}
+
+Where :math:`C_{ld}` is the roll moment damping coefficient, :math:`L_{r}` 
+is the reference length, which is equal to the rocket diameter, and
+:math:`\omega_z` is the angular velocity of the rocket around the z-axis.
+
+Adding Individual Fins to the Rocket
+====================================
+.. jupyter-execute::
+  :hide-code:
+  :hide-output:
+
+  from rocketpy import *
+  env = Environment(latitude=32.990254, longitude=-106.974998, elevation=1400)
+  Pro75M1670 = SolidMotor(
+      thrust_source="../data/motors/cesaroni/Cesaroni_M1670.eng",
+      dry_mass=1.815,
+      dry_inertia=(0.125, 0.125, 0.002),
+      nozzle_radius=33 / 1000,
+      grain_number=5,
+      grain_density=1815,
+      grain_outer_radius=33 / 1000,
+      grain_initial_inner_radius=15 / 1000,
+      grain_initial_height=120 / 1000,
+      grain_separation=5 / 1000,
+      grains_center_of_mass_position=0.397,
+      center_of_dry_mass_position=0.317,
+      nozzle_position=0,
+      burn_time=3.9,
+      throat_radius=11 / 1000,
+      coordinate_system_orientation="nozzle_to_combustion_chamber",
+  )
+  # IMPORTANT: modify the file paths below to match your own system
+
+  example_rocket = Rocket(
+      radius=127 / 2000,
+      mass=14.426,
+      inertia=(6.321, 6.321, 0.034),
+      power_off_drag="../data/rockets/calisto/powerOffDragCurve.csv",
+      power_on_drag="../data/rockets/calisto/powerOnDragCurve.csv",
+      center_of_mass_without_motor=0,
+      coordinate_system_orientation="tail_to_nose",
+  )
+
+  rail_buttons = example_rocket.set_rail_buttons(
+      upper_button_position=0.0818,
+      lower_button_position=-0.618,
+      angular_position=45,
+  )
+  example_rocket.add_motor(Pro75M1670, position=-1.255)
+  nose_cone = example_rocket.add_nose(length=0.55829, kind="vonKarman", position=1.278)
+  tail = example_rocket.add_tail(
+      top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656
+  )
+  example_rocket.add_trapezoidal_fins(
+      n=4,
+      root_chord=0.120,
+      tip_chord=0.060,
+      span=0.110,
+      cant_angle=0.0,
+      position=-1.04956,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+
+Given a defined ``Rocket`` object, we can add individual fins to the rocket by 
+using the ``add_surfaces`` method. Here is an example of adding two canards
+in the Calisto rocket from the :ref:`First Simulation <firstsimulation>` example:
+
+.. jupyter-execute::
+
+  canard1 = TrapezoidalFin(
+      angular_position=0,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+  canard2 = TrapezoidalFin(
+      angular_position=180,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+
+  # Position along the center axis of the rocket is specified here.
+  # If different positions are desired, the position can be specified as a list.
+  example_rocket.add_surfaces([canard1, canard2], positions = 0.35)
+
+  example_rocket.draw(plane="yz")
+
+.. seealso::
+
+  There are three classes for defining fins in RocketPy given their geometry:
+  
+  - :class:`rocketpy.TrapezoidalFin` - For how to define a trapezoidal fin
+  - :class:`rocketpy.EllipticalFin` - For how to define an elliptical fin
+  - :class:`rocketpy.FreeFormFin` - For how to define a free form fin
+
+
+
+Fin Force Conventions
+=====================
+
+.. - Explain positive cant angle resultant force
+.. - if all fins have positive cant angle then they will all generate a force that will rotate the rocket in the same direction
+..   which is negative roll 
+.. - show what a positive and negative cant angle on oposing fins looks like. (generate pitch moment -> pitch control)
+.. - show what a positive and negative cant angle on oposing fins looks like. (generate yaw moment -> yaw control)
+.. - example for 4 fins, show how to count the number of fins and how to access each of them
+
+
+  
+Here we exemplify the fin force conventions relating the cant angle 
+(deflection angle) of the fins to the pitch, yaw and roll moments. We will
+consider a rocket with four fins, to illustrate the concepts. The image below
+show the sign convention for the forces acting on the fins, given positive cant
+angles:
+
+.. image:: ../../static/rocket/fin_forces.png
+   :width: 800
+   :align: center
+
+
+Roll
+^^^^
+
+.. jupyter-execute::
+  :hide-code:
+  :hide-output:
+
+  example_rocket.aerodynamic_surfaces.pop()
+  example_rocket.aerodynamic_surfaces.pop()
+
+
+A positive cant angle :math:`\delta` produces a negative roll moment at zero 
+angle of attack. Any fin with a positive cant angle will produce a negative roll
+moment, and any fin with a negative cant angle will produce a positive roll
+moment.
+
+Here is a flight of the calisto with canards defined with a positive cant angle: 
+
+.. jupyter-execute::
+
+  
+  canard1 = TrapezoidalFin(
+      angular_position=0,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+  canard2 = TrapezoidalFin(
+      angular_position=180,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+
+  example_rocket.add_surfaces([canard1, canard2], positions = 0.35)
+
+  test_flight = Flight(
+      rocket=example_rocket, 
+      environment=env, rail_length=5.2, inclination=85, heading=0,
+      terminate_on_apogee=True,
+  )
+
+  # Rolling Moment 
+  test_flight.M3()
+
+  # Rolling Speed
+  test_flight.w3()
+
+  # Angle of attack
+  test_flight.partial_angle_of_attack.plot(test_flight.out_of_rail_time, 5)
+
+  # Angle of sideslip
+  test_flight.angle_of_sideslip.plot(test_flight.out_of_rail_time, 5)
+
+Pitch
+^^^^^
+
+.. jupyter-execute::
+  :hide-code:
+  :hide-output:
+
+  example_rocket.aerodynamic_surfaces.pop()
+  example_rocket.aerodynamic_surfaces.pop()
+
+Given canards fins at 90 degrees and 270 degrees, having opposite cant angles, 
+a positive pitch moment will be generated. The following example shows the 
+effect of this configuration in the non-zero angle of attack flight of the 
+rocket:
+
+.. jupyter-execute::
+
+  
+  canard1 = TrapezoidalFin(
+      angular_position=90,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+  canard2 = TrapezoidalFin(
+      angular_position=270,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=-0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+
+  example_rocket.add_surfaces([canard1, canard2], positions = 0.35)
+
+  test_flight = Flight(
+      rocket=example_rocket, 
+      environment=env, rail_length=5.2, inclination=85, heading=0,
+      terminate_on_apogee=True,
+  )
+
+  # Angle of attack
+  test_flight.partial_angle_of_attack.plot(test_flight.out_of_rail_time, 5)
+
+  # Angle of sideslip
+  test_flight.angle_of_sideslip.plot(test_flight.out_of_rail_time, 5)
+
+Yaw
+^^^
+
+.. jupyter-execute::
+  :hide-code:
+  :hide-output:
+
+  example_rocket.aerodynamic_surfaces.pop()
+  example_rocket.aerodynamic_surfaces.pop()
+
+Given opposing canards at 0 degrees and 180 degrees, having opposite cant angles, 
+a positive yaw moment will be generated. The following example shows the 
+effect of this configuration in the non-zero angle of attack flight of the 
+rocket:
+
+.. jupyter-execute::
+
+  
+  canard1 = TrapezoidalFin(
+      angular_position=0,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+  canard2 = TrapezoidalFin(
+      angular_position=180,
+      root_chord=0.060,
+      tip_chord=0.020,
+      span=0.03,
+      rocket_radius=example_rocket.radius,
+      cant_angle=-0.5,
+      airfoil=("../data/airfoils/NACA0012-radians.txt", "radians"),
+  )
+
+  example_rocket.add_surfaces([canard1, canard2], positions = 0.35)
+
+  test_flight = Flight(
+      rocket=example_rocket, 
+      environment=env, rail_length=5.2, inclination=85, heading=0,
+      terminate_on_apogee=True,
+  )
+
+  # Angle of attack
+  test_flight.partial_angle_of_attack.plot(test_flight.out_of_rail_time, 5)
+
+  # Angle of sideslip
+  test_flight.angle_of_sideslip.plot(test_flight.out_of_rail_time, 5)
+
+
+
+
+
diff --git a/docs/technical/index.rst b/docs/technical/index.rst
index b96e611ed..73583eba9 100644
--- a/docs/technical/index.rst
+++ b/docs/technical/index.rst
@@ -13,6 +13,7 @@ in their code.
    Equations of Motion v0 <equations_of_motion.rst>
    Equations of Motion v1 <equations_of_motion_v1.rst>
    Elliptical Fins <aerodynamics/elliptical_fins.rst>
+   Individual Fin <aerodynamics/individual_fins.rst>
    Roll Moment <aerodynamics/roll_equations.rst>
    Sensitivity Analysis <sensitivity.rst>
    References <references.rst>
diff --git a/docs/user/aerodynamics/surfaces.rst b/docs/user/aerodynamics/surfaces.rst
new file mode 100644
index 000000000..38f266dca
--- /dev/null
+++ b/docs/user/aerodynamics/surfaces.rst
@@ -0,0 +1,350 @@
+.. _aerodynamic_surfaces:
+
+====================
+Aerodynamic Surfaces
+====================
+
+This page provides an overview of the aerodynamic surfaces available in
+RocketPy and explains how they connect to the rocket's simulation.
+
+RocketPy models the aerodynamic forces and moments generated by three types
+of surfaces: **nose cones**, **fins**, and **tails**. Each surface is
+defined by its geometric parameters and, optionally, by an airfoil profile.
+The aerodynamic coefficients are computed internally using the Barrowman
+method and are used during the flight simulation to evaluate the rocket's
+stability and control.
+
+.. seealso::
+
+   For the full mathematical derivations of the Barrowman method applied to
+   individual fins, see :doc:`Individual Fin Model </technical/aerodynamics/individual_fins>`.
+
+   For the elliptical fin equations, see
+   :doc:`Elliptical Fins Equations </technical/aerodynamics/elliptical_fins>`.
+
+   For roll dynamics and cant angle conventions, see
+   :doc:`Roll Equations </technical/aerodynamics/roll_equations>`.
+
+   For the coordinate systems used by the Rocket class, see
+   :doc:`Rocket Class Axes Definitions </user/rocket/rocket_axes>` and
+   :doc:`Positions and Coordinate Systems </user/positions>`.
+
+Nose Cones
+==========
+
+The nose cone is the forward-most aerodynamic surface of the rocket. It
+contributes to the normal force and the center of pressure position.
+
+Available Nose Cone Kinds
+-------------------------
+
+RocketPy supports the following nose cone shapes, specified via the ``kind``
+parameter:
+
+- ``"conical"``: A simple cone with a straight taper from base to tip.
+- ``"ogive"``: A tangent ogive shape, defined by the ratio of the tip
+  radius to the base radius (the ``bluffness`` parameter).
+- ``"elliptical"``: An elliptical cross-section nose cone.
+- ``"tangent"``: A tangent ogive with a rounded tip.
+- ``"von karman"``: A Von Karman ogive, a common choice for supersonic
+  rockets.
+- ``"parabolic"``: A parabolic nose cone shape.
+- ``"powerseries"``: A power series nose cone, controlled by the
+  ``power`` parameter (must be between 0 and 1). When this kind is used,
+  the ``bluffness`` parameter must be ``None`` or ``0``.
+- ``"lvhaack"``: A LV-Haack series nose cone.
+
+.. note::
+
+   The ``bluffness`` parameter controls the ratio between the radius of
+   the rounded tip and the radius of the base. It is only used for ogive
+   nose cones. For all other kinds, it should be ``None`` or ``0``.
+
+.. caution::
+
+   When ``kind="powerseries"``, the ``power`` parameter is required and
+   must satisfy ``0 < power <= 1``. A value of 1 produces a conical shape,
+   while lower values produce blunter shapes.
+
+Geometric Parameters
+--------------------
+
+All nose cones share the following parameters:
+
+- ``length``: The length of the nose cone along the rocket's centerline.
+- ``base_radius``: The radius of the nose cone at its base, which must
+  match the rocket's radius at the nose cone position.
+- ``position``: The position of the nose cone along the rocket's
+  centerline, relative to the coordinate system origin. See
+  :doc:`Positions and Coordinate Systems </user/positions>` for details.
+
+The center of pressure of the nose cone is computed internally and
+contributes to the overall aerodynamic model. The normal force coefficient
+derivative (CLalpha) depends on the nose cone kind and geometry.
+
+.. seealso::
+
+   For the class API, see :class:`rocketpy.NoseCone`.
+
+Fins
+====
+
+Fins are the primary stabilizing surfaces of a rocket. RocketPy supports
+three fin geometries and two ways to define them: as a **fin set** (the
+usual approach) or as an **individual fin**.
+
+Fin Sets vs. Individual Fins
+-----------------------------
+
+RocketPy distinguishes between two levels of fin definition:
+
+- **Fin set classes** (:class:`rocketpy.TrapezoidalFins`,
+  :class:`rocketpy.EllipticalFins`,
+  :class:`rocketpy.FreeFormFins`): These classes define a *set* of N
+  fins arranged symmetrically around the rocket. The aerodynamic
+  coefficients are computed using the Barrowman method, which accounts for
+  fin-body interference. This is the most common way to define fins.
+
+- **Individual fin classes** (:class:`rocketpy.TrapezoidalFin`,
+  :class:`rocketpy.EllipticalFin`,
+  :class:`rocketpy.FreeFormFin`): These classes define a *single* fin.
+  The moment coefficients are derived differently and are documented
+  separately. Individual fins are useful for canards, asymmetric
+  configurations, or when you need fine-grained control.
+
+.. seealso::
+
+   For the mathematical model of individual fins, including the moment
+   coefficient derivations, see
+   :doc:`Individual Fin Model </technical/aerodynamics/individual_fins>`.
+
+Fin Geometries
+--------------
+
+Trapezoidal Fins
+~~~~~~~~~~~~~~~~
+
+Trapezoidal fins are defined by a root chord, tip chord, span, and
+optionally a sweep length. They are the most common fin geometry in
+model rocketry.
+
+Parameters:
+
+- ``root_chord``: The chord length at the fin's root (where it meets the
+  rocket body).
+- ``tip_chord``: The chord length at the fin's tip. Setting this to 0
+  produces a triangular fin.
+- ``span``: The span of the fin, measured from the rocket body to the
+  fin tip.
+- ``sweep_length`` (optional): The distance from the root chord leading
+  edge to the tip chord leading edge, measured along the rocket's
+  centerline. If not provided, it is computed from the root chord, tip
+  chord, and span.
+- ``cant_angle`` (optional): The angle at which the fin is canted
+  relative to the rocket's centerline, in radians. A positive cant angle
+  produces a negative roll moment at zero angle of attack.
+
+.. caution::
+
+   The ``cant_angle`` convention is important for control surface design.
+   See :doc:`Roll Equations </technical/aerodynamics/roll_equations>` for
+   details on how cant angles affect roll, pitch, and yaw moments.
+
+Elliptical Fins
+~~~~~~~~~~~~~~~
+
+Elliptical fins are defined by a root chord and a span. The chord length
+varies elliptically from root to tip.
+
+Parameters:
+
+- ``root_chord``: The chord length at the fin's root.
+- ``span``: The span of the fin.
+
+.. seealso::
+
+   For the full mathematical derivation, see
+   :doc:`Elliptical Fins Equations </technical/aerodynamics/elliptical_fins>`.
+
+Free Form Fins
+~~~~~~~~~~~~~~
+
+Free form fins allow arbitrary fin shapes defined by a list of
+``(x, y)`` coordinates. This is useful for non-standard fin geometries
+that cannot be represented by trapezoidal or elliptical shapes.
+
+Parameters:
+
+- ``coordinates``: A list of ``(x, y)`` tuples defining the fin shape
+  in the fin coordinate frame.
+
+Common Fin Set Parameters
+-------------------------
+
+In addition to the geometry-specific parameters above, all fin sets
+share the following:
+
+- ``n``: The number of fins in the set (for fin set classes only).
+- ``position``: The position of the fin set along the rocket's
+  centerline, relative to the coordinate system origin.
+- ``angular_position`` (optional): The roll angle of the first fin in
+  the set, in degrees. Measured from the y-axis of the rocket's
+  coordinate system.
+- ``rocket_radius``: The radius of the rocket at the fin's position.
+  This is usually set automatically when adding fins to a rocket.
+- ``airfoil`` (optional): A tuple ``(path, units)`` specifying an
+  airfoil profile. See :ref:`airfoil_profiles` below.
+
+.. _airfoil_profiles:
+
+Airfoil Profiles
+----------------
+
+Fin aerodynamic coefficients can be enhanced by specifying an airfoil
+profile. Without an airfoil, fins are treated as flat plates.
+
+The ``airfoil`` parameter accepts a tuple of the form ``(path, units)``:
+
+- ``path``: Path to a CSV file containing the airfoil's lift coefficient
+  curve. The first column is the angle of attack, the second column is
+  the lift coefficient (CL).
+- ``units``: The unit of the angle of attack in the CSV file. Must be
+  either ``"radians"`` or ``"degrees"``.
+
+The CSV file should contain angle of attack points up to the stall point.
+The data is used to compute the fin's CLalpha (normal force coefficient
+derivative) during the simulation.
+
+.. note::
+
+   If ``airfoil`` is not provided or is ``None``, the fin is modeled as
+   a flat plate. This is a reasonable approximation for many model
+   rockets but may underestimate the normal force coefficient.
+
+.. seealso::
+
+   Airfoil data files can be obtained from
+   `Airfoil Tools <http://airfoiltools.com/>`_.
+
+Adding Fins to a Rocket
+-----------------------
+
+Fins can be added to a rocket using the ``Rocket`` class methods:
+
+.. code-block:: python
+
+   from rocketpy import Rocket, TrapezoidalFins
+
+   rocket = Rocket(
+       radius=0.0635,
+       mass=14.426,
+       inertia=(6.321, 6.321, 0.034),
+       power_off_drag="data/powerOffDragCurve.csv",
+       power_on_drag="data/powerOnDragCurve.csv",
+       center_of_mass_without_motor=0,
+       coordinate_system_orientation="tail_to_nose",
+   )
+
+   fin_set = rocket.add_trapezoidal_fins(
+       n=4,
+       root_chord=0.120,
+       tip_chord=0.060,
+       span=0.110,
+       position=-1.04956,
+       cant_angle=0.0,
+       airfoil=("data/airfoils/NACA0012-radians.txt", "radians"),
+   )
+
+.. seealso::
+
+   - :meth:`rocketpy.Rocket.add_trapezoidal_fins`
+   - :meth:`rocketpy.Rocket.add_elliptical_fins`
+   - :meth:`rocketpy.Rocket.add_free_form_fins`
+   - :meth:`rocketpy.Rocket.add_surfaces` (for individual fins)
+
+Tail
+====
+
+The tail is a transitional surface at the aft end of the rocket, typically
+used to reduce base drag. It is defined by a top radius, bottom radius,
+and length.
+
+Parameters:
+
+- ``top_radius``: The radius of the tail at its top (where it meets the
+  rocket body).
+- ``bottom_radius``: The radius of the tail at its bottom (aft end).
+- ``length``: The length of the tail along the rocket's centerline.
+- ``position``: The position of the tail along the rocket's centerline.
+
+The tail contributes to the normal force and center of pressure
+calculation. Its effect is generally smaller than that of the nose cone
+and fins.
+
+.. seealso::
+
+   For the class API, see :class:`rocketpy.Tail`.
+
+Generic Surfaces
+================
+
+For advanced use cases, RocketPy provides the
+:class:`rocketpy.GenericSurface` and
+:class:`rocketpy.LinearGenericSurface` classes. These allow you to
+specify aerodynamic force and moment coefficients directly, rather than
+relying on the built-in geometric models.
+
+This is useful when:
+
+- You have aerodynamic data from CFD simulations or wind tunnel tests.
+- You want to model aerodynamic surfaces that do not fit the built-in
+  geometries (e.g., canards with unusual shapes, air brakes).
+
+.. seealso::
+
+   For more information, see
+   :doc:`Generic Surfaces and Custom Aerodynamic Coefficients </user/rocket/generic_surface>`.
+
+.. note::
+
+   This section provides a brief overview of generic surfaces. A more
+   detailed treatment of coordinate frames and coefficient conventions
+   for generic surfaces is available in the referenced user guide page.
+
+Reference Area and Length
+=========================
+
+The aerodynamic forces and moments computed by each surface are scaled by
+a reference area and a reference length:
+
+- **Reference area**: The cross-sectional area of the rocket, computed
+  as :math:`\pi r^2` where :math:`r` is the rocket's radius.
+- **Reference length**: The diameter of the rocket (:math:`2r`).
+
+These values are used consistently across all aerodynamic surfaces and
+are set automatically from the rocket's radius.
+
+.. seealso::
+
+   For more details on how forces and moments are applied during the
+   simulation, see :class:`rocketpy.Rocket` and
+   :class:`rocketpy.Flight`.
+
+What's Next
+============
+
+This page covers the available surface types and their parameters. For
+deeper understanding of the underlying math:
+
+- :doc:`Individual Fin Model </technical/aerodynamics/individual_fins>`:
+  Full derivation of the Barrowman method for individual fins, including
+  moment coefficients.
+- :doc:`Elliptical Fins Equations </technical/aerodynamics/elliptical_fins>`:
+  Geometric parameters and center of pressure for elliptical fins.
+- :doc:`Roll Equations </technical/aerodynamics/roll_equations>`:
+  Roll moment and damping equations for high-powered rockets.
+
+For coordinate system conventions:
+
+- :doc:`Rocket Class Axes Definitions </user/rocket/rocket_axes>`
+- :doc:`Positions and Coordinate Systems </user/positions>`
diff --git a/docs/user/airbrakes.rst b/docs/user/airbrakes.rst
index 97d39ba59..5d47d4d6b 100644
--- a/docs/user/airbrakes.rst
+++ b/docs/user/airbrakes.rst
@@ -95,60 +95,23 @@ To create an air brakes model, we essentially need to define the following:
   ``deployment_level`` attribute. Inside this function, any controller logic,
   filters, and apogee prediction can be implemented.
 
-- The **sampling rate** of the controller function, in seconds. This is the time
-  between each call of the controller function, in simulation time. Must be
-  given in Hertz.
+- The **sampling rate** of the controller function, in Hertz. This is how often
+  the controller function is called in simulation time (a **discrete**
+  controller). It can also be set to ``None`` to create a **continuous**
+  controller that is called at every solver step (see
+  :ref:`discrete-vs-continuous-controllers` below).
 
 Defining the Controller Function
 ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
 
 Lets start by defining a very simple controller function.
 
-The ``controller_function`` must take in the following arguments, in this
-order:
-
-1. ``time`` (float): The current simulation time in seconds.
-2. ``sampling_rate`` (float): The rate at which the controller
-   function is called, measured in Hertz (Hz).
-3. ``state`` (list): The state vector of the simulation. The state
-   is a list containing the following values, in this order:
-
-   - ``x``: The x position of the rocket, in meters.
-   - ``y``: The y position of the rocket, in meters.
-   - ``z``: The z position of the rocket, in meters.
-   - ``v_x``: The x component of the velocity of the rocket, in meters per
-     second.
-   - ``v_y``: The y component of the velocity of the rocket, in meters per
-     second.
-   - ``v_z``: The z component of the velocity of the rocket, in meters per
-     second.
-   - ``e0``: The first component of the quaternion representing the rotation
-     of the rocket.
-   - ``e1``: The second component of the quaternion representing the rotation
-     of the rocket.
-   - ``e2``: The third component of the quaternion representing the rotation
-     of the rocket.
-   - ``e3``: The fourth component of the quaternion representing the rotation
-     of the rocket.
-   - ``w_x``: The x component of the angular velocity of the rocket, in
-     radians per second.
-   - ``w_y``: The y component of the angular velocity of the rocket, in
-     radians per second.
-   - ``w_z``: The z component of the angular velocity of the rocket, in
-     radians per second.
-
-4. ``state_history`` (list): A record of the rocket's state at each
-   step throughout the simulation. The state_history is organized as
-   a list of lists, with each sublist containing a state vector. The
-   last item in the list always corresponds to the previous state
-   vector, providing a chronological sequence of the rocket's
-   evolving states.
-5. ``observed_variables`` (list): A list containing the variables that
-   the controller function returns. The return of each controller
-   function call is appended to the observed_variables list. The
-   initial value in the first step of the simulation of this list is
-   provided by the ``initial_observed_variables`` argument.
-6. ``air_brakes`` (AirBrakes): The ``AirBrakes`` instance being controlled.
+The ``controller_function`` receives information about the simulation at the
+current time step and sets the air brakes' deployment level. See
+:ref:`controllers` for the full description of its arguments and call signature.
+For air brakes, the controlled object (the ``air_brakes`` argument) is the
+:class:`rocketpy.AirBrakes` instance, whose ``deployment_level`` the function
+sets.
 
 Our example ``controller_function`` will deploy the air brakes when the rocket
 reaches 1500 meters above the ground. The deployment level will be function of the
@@ -224,22 +187,6 @@ Lets define the controller function:
 
 .. note::
 
-    - The ``controller_function`` accepts 6, 7, or 8 parameters for backward
-      compatibility:
-
-      * **6 parameters** (original): ``time``, ``sampling_rate``, ``state``,
-        ``state_history``, ``observed_variables``, ``air_brakes``
-      * **7 parameters** (with sensors): adds ``sensors`` as the 7th parameter
-      * **8 parameters** (with environment): adds ``sensors`` and ``environment``
-        as the 7th and 8th parameters
-
-    - The **environment parameter** provides access to atmospheric conditions
-      (wind, temperature, pressure, elevation) without relying on global variables.
-      This enables proper serialization of rockets with air brakes and improves
-      code modularity. Available methods include ``environment.elevation``,
-      ``environment.wind_velocity_x(altitude)``, ``environment.wind_velocity_y(altitude)``,
-      ``environment.speed_of_sound(altitude)``, and others.
-
     - The code inside the ``controller_function`` can be as complex as needed.
       Anything can be implemented inside the function, including filters,
       apogee prediction, and any controller logic.
@@ -249,15 +196,10 @@ Lets define the controller function:
       0 or higher than 1. If you want to disable this feature, set ``clamp`` to
       ``False`` when defining the air brakes.
 
-    - Anything can be returned by the ``controller_function``. The returned
-      values will be saved in the ``observed_variables`` list at every time step
-      and can then be accessed by the ``controller_function`` at the next time
-      step. The saved values can also be accessed after the simulation is
-      finished. This is useful for debugging and for plotting the results.
-
-    - The ``controller_function`` can also be defined in a separate file and
-      imported into the simulation script. This includes importing a ``c`` or
-      ``cpp`` code into Python.
+    - See :ref:`controllers` for the controller-function signature (including the
+      6/7/8-parameter forms and the ``environment`` argument), how returned
+      values are stored in ``observed_variables``, and discrete vs. continuous
+      controllers.
 
 
 Defining the Drag Coefficient
@@ -372,6 +314,15 @@ controller function. If you want to disable this feature, set ``clamp`` to
     For more information on the :class:`rocketpy.AirBrakes` class
     initialization, see  :class:`rocketpy.AirBrakes.__init__` section.
 
+.. note::
+
+    Because our controller uses ``sampling_rate=10``, it is a **discrete**
+    controller and adds its sampling instants as time nodes to the simulation.
+    Remember to set ``time_overshoot=False`` in the ``Flight`` (see below) so the
+    integrator stops exactly at those instants. See
+    :ref:`discrete-vs-continuous-controllers` for the difference between discrete
+    and continuous controllers.
+
 Simulating a Flight
 -------------------
 
diff --git a/docs/user/compare_flights.rst b/docs/user/compare_flights.rst
index d7f8478c8..c352e8b19 100644
--- a/docs/user/compare_flights.rst
+++ b/docs/user/compare_flights.rst
@@ -14,7 +14,7 @@ We will start by importing the necessary classes and modules:
 .. jupyter-execute::
 
       from rocketpy.plots.compare import CompareFlights
-      from rocketpy import Environment, Flight, Rocket, SolidMotor
+      from rocketpy import Environment, Flight, Rocket, SolidMotor, HemisphericalParachute
       from datetime import datetime, timedelta
 
 
@@ -83,7 +83,7 @@ This is done following the same steps as in the :ref:`firstsimulation` example.
           top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656
       )
 
-      main_chute = calisto.add_parachute(
+      main_chute = HemisphericalParachute(
           "Main",
           cd_s=10.0,
           trigger=800,
@@ -92,7 +92,7 @@ This is done following the same steps as in the :ref:`firstsimulation` example.
           noise=(0, 8.3, 0.5),
       )
 
-      drogue_chute = calisto.add_parachute(
+      drogue_chute = HemisphericalParachute(
           "Drogue",
           cd_s=1.0,
           trigger="apogee",
@@ -100,6 +100,8 @@ This is done following the same steps as in the :ref:`firstsimulation` example.
           lag=1.5,
           noise=(0, 8.3, 0.5),
       )
+      calisto.add_parachute(parachute = main_chute)
+      calisto.add_parachute(parachute = drogue_chute)
 
 Creating the Flight objects
 ---------------------------
diff --git a/docs/user/controllers.rst b/docs/user/controllers.rst
new file mode 100644
index 000000000..0b866dfb0
--- /dev/null
+++ b/docs/user/controllers.rst
@@ -0,0 +1,132 @@
+.. _controllers:
+
+Controllers
+===========
+
+RocketPy can simulate active, in-flight control systems — such as air brakes or
+other actuators — through a *controller function* that you attach to a
+controllable object (for example, an :class:`rocketpy.AirBrakes` added with
+``Rocket.add_air_brakes``). During the flight simulation, RocketPy calls your
+controller function at the appropriate times, letting it read the current
+simulation state and command the actuator.
+
+This page describes the controller-function interface and how its call timing is
+governed. For a complete, runnable example that puts these pieces together, see
+the :doc:`Air Brakes Example <airbrakes>`.
+
+The Controller Function
+-----------------------
+
+A controller function receives information about the simulation up to the
+current time step and sets the state of the controlled object. It must take in
+the following arguments, in this order:
+
+1. ``time`` (float): The current simulation time in seconds.
+2. ``sampling_rate`` (float or ``None``): The rate at which the controller
+   function is called, measured in Hertz (Hz). It is ``None`` for continuous
+   controllers, so guard any ``1 / sampling_rate`` computation against ``None``.
+3. ``state`` (list): The state vector of the simulation. The state
+   is a list containing the following values, in this order:
+
+   - ``x``: The x position of the rocket, in meters.
+   - ``y``: The y position of the rocket, in meters.
+   - ``z``: The z position of the rocket, in meters.
+   - ``v_x``: The x component of the velocity of the rocket, in meters per
+     second.
+   - ``v_y``: The y component of the velocity of the rocket, in meters per
+     second.
+   - ``v_z``: The z component of the velocity of the rocket, in meters per
+     second.
+   - ``e0``: The first component of the quaternion representing the rotation
+     of the rocket.
+   - ``e1``: The second component of the quaternion representing the rotation
+     of the rocket.
+   - ``e2``: The third component of the quaternion representing the rotation
+     of the rocket.
+   - ``e3``: The fourth component of the quaternion representing the rotation
+     of the rocket.
+   - ``w_x``: The x component of the angular velocity of the rocket, in
+     radians per second.
+   - ``w_y``: The y component of the angular velocity of the rocket, in
+     radians per second.
+   - ``w_z``: The z component of the angular velocity of the rocket, in
+     radians per second.
+
+4. ``state_history`` (list): A record of the rocket's state at each
+   step throughout the simulation. The state_history is organized as
+   a list of lists, with each sublist containing a state vector. The
+   last item in the list always corresponds to the previous state
+   vector, providing a chronological sequence of the rocket's
+   evolving states.
+5. ``observed_variables`` (list): A list containing the variables that
+   the controller function returns. The return of each controller
+   function call is appended to the observed_variables list. The
+   initial value in the first step of the simulation of this list is
+   provided by the ``initial_observed_variables`` argument.
+6. The **controlled object** (e.g. ``air_brakes``): the instance being
+   controlled, whose attributes the function sets (for example,
+   ``air_brakes.deployment_level``).
+
+.. note::
+
+    - The controller function accepts 6, 7, or 8 parameters for backward
+      compatibility:
+
+      * **6 parameters** (original): ``time``, ``sampling_rate``, ``state``,
+        ``state_history``, ``observed_variables``, and the controlled object.
+      * **7 parameters** (with sensors): adds ``sensors`` as the 7th parameter.
+      * **8 parameters** (with environment): adds ``sensors`` and ``environment``
+        as the 7th and 8th parameters.
+
+    - The **environment parameter** provides access to atmospheric conditions
+      (wind, temperature, pressure, elevation) without relying on global
+      variables. This enables proper serialization of rockets with controllers
+      and improves code modularity. Available methods include
+      ``environment.elevation``, ``environment.wind_velocity_x(altitude)``,
+      ``environment.wind_velocity_y(altitude)``,
+      ``environment.speed_of_sound(altitude)``, and others.
+
+    - Anything can be returned by the controller function. The returned values
+      are saved in the ``observed_variables`` list at every time step and can
+      then be accessed by the controller function at the next time step. The
+      saved values can also be accessed after the simulation is finished, which
+      is useful for debugging and for plotting the results.
+
+    - The controller function can also be defined in a separate file and
+      imported into the simulation script. This includes importing ``c`` or
+      ``cpp`` code into Python.
+
+.. _discrete-vs-continuous-controllers:
+
+Discrete vs. Continuous Controllers
+-----------------------------------
+
+The ``sampling_rate`` argument determines *when* the controller function is
+called during the flight simulation:
+
+- **Discrete controller** (``sampling_rate`` set to a number, e.g. ``10``):
+  the controller function is called at fixed intervals of ``1 / sampling_rate``
+  seconds. This mirrors a real flight computer that reads its sensors and
+  updates its actuators at a fixed frequency, and is the recommended choice
+  when you want the simulation to reflect the actual control-loop rate of your
+  hardware.
+- **Continuous controller** (``sampling_rate=None``): the controller function
+  is called at *every* solver step of the numerical integrator. Use this when
+  you want the control law to act as a continuous function of the state rather
+  than a sampled one (for example, when validating a control model
+  analytically).
+
+.. warning::
+
+    For continuous controllers, ``sampling_rate`` is passed to your controller
+    function as ``None``. Any computation such as ``1 / sampling_rate`` (a
+    common pattern for rate-limiting deployment) must guard against ``None`` to
+    avoid a ``TypeError``.
+
+.. note::
+
+    Discrete controllers add their sampling instants as time nodes to the
+    simulation, so remember to set ``time_overshoot=False`` in the ``Flight``
+    to make the integrator stop exactly at those instants. Continuous
+    controllers do not add time nodes; they are evaluated on the integrator's
+    own steps.
diff --git a/docs/user/deployable.rst b/docs/user/deployable.rst
index cd9a7a97b..ddc082a6f 100644
--- a/docs/user/deployable.rst
+++ b/docs/user/deployable.rst
@@ -8,7 +8,7 @@ Let's start by importing the rocketpy classes we will use.
 
 .. jupyter-execute::
 
-      from rocketpy import Environment, SolidMotor, Rocket, Flight
+      from rocketpy import Environment, SolidMotor, Rocket, Flight, HemisphericalParachute
 
 
 Creating Environment
@@ -182,7 +182,7 @@ Therefore we should be careful with the value of its mass.
 
 
       # Define Parachutes for the rocket
-      main_chute = rocket_without_payload.add_parachute(
+      main_chute = HemisphericalParachute(
           "Main",
           cd_s=7.2,
           trigger=800,
@@ -191,7 +191,7 @@ Therefore we should be careful with the value of its mass.
           noise=(0, 8.3, 0.5),
       )
 
-      drogue_chute = rocket_without_payload.add_parachute(
+      drogue_chute = HemisphericalParachute(
           "Drogue",
           cd_s=0.72,
           trigger="apogee",
@@ -199,6 +199,8 @@ Therefore we should be careful with the value of its mass.
           lag=1.5,
           noise=(0, 8.3, 0.5),
       )
+      rocket_without_payload.add_parachute(parachute = main_chute)
+      rocket_without_payload.add_parachute(parachute = drogue_chute)
 
 .. jupyter-execute::
 
@@ -242,7 +244,7 @@ surfaces to stabilize it, nor a motor that ignites. It does, however, have parac
           center_of_mass_without_motor=0,
       )
 
-      payload_drogue = payload_rocket.add_parachute(
+      payload_drogue = HemisphericalParachute(
           "Drogue",
           cd_s=0.35,
           trigger="apogee",
@@ -251,7 +253,7 @@ surfaces to stabilize it, nor a motor that ignites. It does, however, have parac
           noise=(0, 8.3, 0.5),
       )
 
-      payload_main = payload_rocket.add_parachute(
+      payload_main = HemisphericalParachute(
           "Main",
           cd_s=4.0,
           trigger=800,
@@ -259,6 +261,8 @@ surfaces to stabilize it, nor a motor that ignites. It does, however, have parac
           lag=1.5,
           noise=(0, 8.3, 0.5),
       )
+      payload_rocket.add_parachute(parachute = payload_drogue)
+      payload_rocket.add_parachute(parachute = payload_main)
 
 .. important::
 
diff --git a/docs/user/environment/1-atm-models/ensemble.rst b/docs/user/environment/1-atm-models/ensemble.rst
index 504cbfe60..8dffaac00 100644
--- a/docs/user/environment/1-atm-models/ensemble.rst
+++ b/docs/user/environment/1-atm-models/ensemble.rst
@@ -25,8 +25,8 @@ Global Ensemble Forecast System (GEFS)
 
 .. danger::
 
-    **GEFS shortcut unavailable**: ``file="GEFS"`` is currently disabled in
-    RocketPy because NOMADS OPeNDAP is deactivated for this endpoint.
+    **GEFS unavailable**: ``file="GEFS"`` is currently disabled in
+    RocketPy because NOMADS OPeNDAP has been deactivated.
 
 .. note::
 
diff --git a/docs/user/environment/1-atm-models/forecast.rst b/docs/user/environment/1-atm-models/forecast.rst
index ac91504e0..ea81c356a 100644
--- a/docs/user/environment/1-atm-models/forecast.rst
+++ b/docs/user/environment/1-atm-models/forecast.rst
@@ -6,8 +6,8 @@ Forecasts
 Weather forecasts can be used to set the atmospheric model in RocketPy.
 
 Here, we will showcase how to import global forecasts such as GFS, as well as
-local forecasts like NAM and RAP for North America, all available through
-OPeNDAP on the `NOAA's NCEP NOMADS <http://nomads.ncep.noaa.gov/>`_ website.
+local forecasts like NAM, RAP and HRRR for North America, all available through
+OPeNDAP on the `UCAR THREDDS <https://thredds.ucar.edu/>`_ server.
 Other generic forecasts can also be imported.
 
 .. important::
@@ -22,6 +22,10 @@ Other generic forecasts can also be imported.
 Global Forecast System (GFS)
 ----------------------------
 
+GFS is NOAA's global numerical weather prediction model. It provides worldwide
+atmospheric forecasts and is usually a good default choice when you need broad
+coverage, consistent availability, and launch planning several days ahead.
+
 Using the latest forecast from GFS is simple.
 Set the atmospheric model to ``forecast`` and specify that GFS is the file you want.
 Note that since data is downloaded from a remote OPeNDAP server, this line of code can
@@ -48,9 +52,34 @@ take longer than usual.
     `GFS overview page <https://www.emc.ncep.noaa.gov/emc/pages/numerical_forecast_systems/gfs.php>`_.
 
 
+Artificial Intelligence Global Forecast System (AIGFS)
+------------------------------------------------------
+
+AIGFS is a global AI-based forecast product distributed through the same THREDDS
+ecosystem used by other RocketPy forecast inputs. It is useful when you want a
+global forecast alternative to traditional physics-only models.
+
+RocketPy supports the latest AIGFS global forecast through THREDDS.
+
+.. jupyter-execute::
+
+    env_aigfs = Environment(date=tomorrow)
+    env_aigfs.set_atmospheric_model(type="forecast", file="AIGFS")
+    env_aigfs.plots.atmospheric_model()
+
+.. note::
+
+    AIGFS is currently available as a global 0.25 degree forecast product on
+    UCAR THREDDS.
+
+
 North American Mesoscale Forecast System (NAM)
 ----------------------------------------------
 
+NAM is a regional forecast model focused on North America. It is best suited
+for launches inside its coverage area when you want finer regional detail than
+global models typically provide.
+
 You can also request the latest forecasts from NAM.
 Since this is a regional model for North America, you need to specify latitude
 and longitude points within North America.
@@ -78,6 +107,10 @@ We will use **SpacePort America** for this, represented by coordinates
 Rapid Refresh (RAP)
 -------------------
 
+RAP is a short-range, high-frequency regional model for North America. It is
+especially useful for near-term operations, where fast update cycles are more
+important than long forecast horizon.
+
 The Rapid Refresh (RAP) model is another regional model for North America.
 It is similar to NAM, but with a higher resolution and a shorter forecast range.
 The same coordinates for SpacePort America will be used.
@@ -111,6 +144,17 @@ The same coordinates for SpacePort America will be used.
 High Resolution Window (HIRESW)
 -------------------------------
 
+HIRESW is a convection-allowing, high-resolution regional system designed to
+resolve local weather structure better than coarser grids. It is most useful
+for short-range, local analysis where small-scale wind and weather features
+matter.
+
+The High Resolution Window (HIRESW) model is a sophisticated weather forecasting
+system that operates at a high spatial resolution of approximately 3 km.
+It utilizes two main dynamical cores: the Advanced Research WRF (WRF-ARW) and
+the Finite Volume Cubed Sphere (FV3), each designed to enhance the accuracy of
+weather predictions.
+
 .. danger::
 
     **HIRESW shortcut unavailable**: ``file="HIRESW"`` is currently disabled in
@@ -121,6 +165,33 @@ you can still load it explicitly by passing the path/URL in ``file`` and an
 appropriate mapping in ``dictionary``.
 
 
+High-Resolution Rapid Refresh (HRRR)
+------------------------------------
+
+HRRR is a high-resolution, short-range forecast model for North America with
+hourly updates. It is generally best for day-of-launch weather assessment and
+rapidly changing local conditions.
+
+RocketPy supports HRRR through a dedicated THREDDS shortcut.
+Like NAM and RAP, HRRR is a regional model over North America, so you need to
+specify latitude and longitude points within its coverage area. The same
+SpacePort America coordinates used above will be reused here.
+
+.. code-block:: python
+
+    env_hrrr = Environment(
+        date=tomorrow,
+        latitude=32.988528,
+        longitude=-106.975056,
+    )
+    env_hrrr.set_atmospheric_model(type="forecast", file="HRRR")
+    env_hrrr.plots.atmospheric_model()
+
+.. note::
+
+    HRRR is a high-resolution regional model with approximately 2.5 km grid
+    spacing over CONUS. Availability depends on upstream THREDDS data services.
+
 
 Using Windy Atmosphere
 ----------------------
@@ -154,6 +225,10 @@ to EuRoC's launch area in Portugal.
 ECMWF
 ^^^^^
 
+ECMWF (HRES) is a global, high-skill forecast model known for strong
+medium-range performance. It is often a good choice for mission planning when
+you need reliable synoptic-scale forecasts several days ahead.
+
 We can use the ``ECMWF`` model from Windy.com. 
 
 .. jupyter-execute::
@@ -173,6 +248,10 @@ We can use the ``ECMWF`` model from Windy.com.
 GFS
 ^^^
 
+Windy's GFS option provides NOAA's global model through Windy's interface. It
+is a practical baseline for global coverage and for comparing against other
+models when assessing forecast uncertainty.
+
 The ``GFS`` model is also available on Windy.com. This is the same model as
 described in the :ref:`global-forecast-system` section.
 
@@ -186,6 +265,10 @@ described in the :ref:`global-forecast-system` section.
 ICON
 ^^^^
 
+ICON is DWD's global weather model, available in Windy for broad-scale
+forecasting. It is useful as an independent global model source to cross-check
+wind and temperature trends against GFS or ECMWF.
+
 The ICON model is a global weather forecasting model already available on Windy.com.
 
 .. jupyter-execute::
@@ -203,6 +286,10 @@ The ICON model is a global weather forecasting model already available on Windy.
 ICON-EU
 ^^^^^^^
 
+ICON-EU is the regional European configuration of ICON, with higher spatial
+detail over Europe than ICON-Global. It is best for European launch sites when
+regional structure is important.
+
 The ICON-EU model is a regional weather forecasting model available on Windy.com.
 
 .. code-block:: python
@@ -228,4 +315,4 @@ Also, the servers may be down or may face high traffic.
 .. seealso::
 
     To browse available NCEP model collections on UCAR THREDDS, visit
-    `THREDDS NCEP Catalog <https://thredds.ucar.edu/thredds/catalog/grib/NCEP/GFS/Global_0p25deg/catalog.html>`_.
\ No newline at end of file
+    `THREDDS NCEP Catalog <https://thredds.ucar.edu/thredds/catalog/grib/NCEP/GFS/Global_0p25deg/catalog.html>`_.
diff --git a/docs/user/environment/1-atm-models/soundings.rst b/docs/user/environment/1-atm-models/soundings.rst
index 279750df5..39fa57d17 100644
--- a/docs/user/environment/1-atm-models/soundings.rst
+++ b/docs/user/environment/1-atm-models/soundings.rst
@@ -13,20 +13,34 @@ Wyoming Upper Air Soundings
 
 The University of Wyoming - College of Engineering - Department of Atmospheric
 Sciences has a comprehensive collection of atmospheric soundings on their website,
-accessible `here <http://weather.uwyo.edu/upperair/sounding.html>`_.
+accessible `here <https://weather.uwyo.edu/upperair/sounding.shtml>`_.
 
 For this example, we will use the sounding from 83779 SBMT Marte Civ Observations
-at 04 Feb 2019, which can be accessed using this URL:
-http://weather.uwyo.edu/cgi-bin/sounding?region=samer&TYPE=TEXT%3ALIST&YEAR=2019&MONTH=02&FROM=0500&TO=0512&STNM=83779
+at 05 Feb 2019, which can be accessed using this URL:
+https://weather.uwyo.edu/wsgi/sounding?datetime=2019-02-05%2012:00:00&id=83779&type=TEXT:LIST
+
+.. important::
+
+    The University of Wyoming discontinued the legacy
+    ``weather.uwyo.edu/cgi-bin/sounding`` endpoint. URLs in that old format no
+    longer work; use the new ``weather.uwyo.edu/wsgi/sounding`` format shown
+    above, which RocketPy supports since v1.13.0.
 
 
 Initialize a new Environment instance:
 
-.. jupyter-execute::
+.. note::
+
+    The example below is shown as static code (it is not executed during the
+    documentation build) because it requires a live network request to an
+    external University of Wyoming service. Run it locally to fetch the
+    sounding and see the resulting atmospheric plots.
+
+.. code-block:: python
 
     from rocketpy import Environment
 
-    url = "http://weather.uwyo.edu/cgi-bin/sounding?region=samer&TYPE=TEXT%3ALIST&YEAR=2019&MONTH=02&FROM=0500&TO=0512&STNM=83779"
+    url = "https://weather.uwyo.edu/wsgi/sounding?datetime=2019-02-05%2012:00:00&id=83779&type=TEXT:LIST"
 
     env = Environment()
     env.set_atmospheric_model(type="wyoming_sounding", file=url)
@@ -59,7 +73,7 @@ Integrated Global Radiosonde Archive (IGRA).
 
 These options can be retrieved as a text file in GSD format. However,
 RocketPy no longer provides a dedicated ``set_atmospheric_model`` type for
-NOAA RUC Soundings.
+NOAA RUC Soundings, since NOAA has discontinued the OPENDAP service.
 
 .. note::
     
diff --git a/docs/user/environment/3-further/other_apis.rst b/docs/user/environment/3-further/other_apis.rst
index 01d4b9a30..37a9a0949 100644
--- a/docs/user/environment/3-further/other_apis.rst
+++ b/docs/user/environment/3-further/other_apis.rst
@@ -89,8 +89,10 @@ Instead of a custom dictionary, you can pass a built-in mapping name in the
 - ``"ECMWF_v0"``
 - ``"NOAA"``
 - ``"GFS"``
+- ``"AIGFS"``
 - ``"NAM"``
 - ``"RAP"``
+- ``"HRRR"``
 - ``"HIRESW"`` (mapping available; latest-model shortcut currently disabled)
 - ``"GEFS"`` (mapping available; latest-model shortcut currently disabled)
 - ``"MERRA2"``
@@ -116,10 +118,7 @@ legacy aliases:
 - ``"NAM_LEGACY"``
 - ``"NOAA_LEGACY"``
 - ``"RAP_LEGACY"``
-- ``"CMC_LEGACY"``
 - ``"GEFS_LEGACY"``
-- ``"HIRESW_LEGACY"``
-- ``"MERRA2_LEGACY"``
 
 Legacy aliases primarily cover older variable naming patterns such as
 ``lev``, ``tmpprs``, ``hgtprs``, ``ugrdprs`` and ``vgrdprs``.
diff --git a/docs/user/first_simulation.rst b/docs/user/first_simulation.rst
index 364557891..effa5ce0d 100644
--- a/docs/user/first_simulation.rst
+++ b/docs/user/first_simulation.rst
@@ -67,7 +67,7 @@ we will use from RocketPy:
 
 .. jupyter-execute::
 
-    from rocketpy import Environment, SolidMotor, Rocket, Flight
+    from rocketpy import Environment, SolidMotor, Rocket, Flight, HemisphericalParachute
 
 .. note::
 
@@ -272,7 +272,7 @@ Finally, we can add any number of Parachutes to the ``Rocket`` object.
 
 .. jupyter-execute::
 
-    main = calisto.add_parachute(
+    main = HemisphericalParachute(
         name="main",
         cd_s=10.0,
         trigger=800,      # ejection altitude in meters
@@ -284,7 +284,7 @@ Finally, we can add any number of Parachutes to the ``Rocket`` object.
         porosity=0.0432,
     )
 
-    drogue = calisto.add_parachute(
+    drogue = HemisphericalParachute(
         name="drogue",
         cd_s=1.0,
         trigger="apogee",  # ejection at apogee
@@ -295,6 +295,8 @@ Finally, we can add any number of Parachutes to the ``Rocket`` object.
         height=1.5,
         porosity=0.0432,
     )
+    calisto.add_parachute(parachute = main)
+    calisto.add_parachute(parachute = drogue)
 
 We can then see if the rocket is stable by plotting the static margin:
 
@@ -587,7 +589,7 @@ Use the dedicated exporter class:
 
 .. note::
 
-    The legacy method ``Flight.export_kml`` is deprecated. Use
+    The legacy method ``Flight.export_kml`` was removed in v1.13.0. Use
     :meth:`rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_kml`.
 
 Manipulating results
@@ -687,7 +689,7 @@ by not passing any attribute names:
 
 .. note::
 
-    The legacy method ``Flight.export_data`` is deprecated. Use
+    The legacy method ``Flight.export_data`` was removed in v1.13.0. Use
     :meth:`rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_data`.
 
 Saving and Storing Plots
diff --git a/docs/user/flight.rst b/docs/user/flight.rst
index 31e7ab588..a220554ab 100644
--- a/docs/user/flight.rst
+++ b/docs/user/flight.rst
@@ -274,7 +274,7 @@ During the rail launch phase, RocketPy calculates reaction forces and internal b
 **Rail Button Forces (N):**
 
 - ``rail_button1_normal_force`` : Normal reaction force at upper rail button
-- ``rail_button1_shear_force`` : Shear (tangential) reaction force at upper rail button  
+- ``rail_button1_shear_force`` : Shear (tangential) reaction force at upper rail button
 - ``rail_button2_normal_force`` : Normal reaction force at lower rail button
 - ``rail_button2_shear_force`` : Shear (tangential) reaction force at lower rail button
 
@@ -282,7 +282,7 @@ During the rail launch phase, RocketPy calculates reaction forces and internal b
 
 - ``rail_button1_bending_moment`` : Time-dependent bending moment at upper rail button attachment
 - ``max_rail_button1_bending_moment`` : Maximum absolute bending moment at upper rail button
-- ``rail_button2_bending_moment`` : Time-dependent bending moment at lower rail button attachment  
+- ``rail_button2_bending_moment`` : Time-dependent bending moment at lower rail button attachment
 - ``max_rail_button2_bending_moment`` : Maximum absolute bending moment at lower rail button
 
 **Calculation Method:**
@@ -454,6 +454,122 @@ Flight Data Plots
     # Flight path and orientation
     flight.plots.flight_path_angle_data()
 
+3D Flight Animation
+~~~~~~~~~~~~~~~~~~~
+
+RocketPy can produce real-time interactive 3D animations of the simulated
+flight using `vedo <https://vedo.embl.es/>`_, a scientific visualization
+library built on top of VTK.  Two complementary animation modes are provided:
+
+.. list-table::
+   :header-rows: 1
+   :widths: 30 70
+
+   * - Method
+     - What it shows
+   * - ``flight.plots.animate_trajectory()``
+     - The rocket 3D model moves through space following the simulated
+       trajectory; a black trail line is drawn behind it.
+   * - ``flight.plots.animate_rotate()``
+     - The rocket 3D model stays centred in the scene; only its attitude
+       (orientation derived from the quaternion solution) is animated.
+
+.. note::
+
+    The animation window opens on the desktop via VTK.  It will **not** render
+    inside headless environments such as Google Colab.  For notebook use, run
+    the cell on a local Jupyter server or JupyterLab installation.
+
+**Installation**
+
+The ``vedo`` dependency is not installed by default.  Add the optional extra
+before calling either animation method:
+
+.. code-block:: bash
+
+    pip install rocketpy[animation]
+
+If ``vedo`` is not available when an animation method is called, RocketPy
+raises an :class:`ImportError` with the above install command embedded in the
+message.
+
+**animate_trajectory — full 6-DOF trajectory animation**
+
+.. code-block:: python
+
+    # Quickstart: uses RocketPy's built-in default STL rocket model
+    flight.plots.animate_trajectory()
+
+    # Customise the time window and frame rate
+    flight.plots.animate_trajectory(
+        start=0.0,                    # start time in seconds (default: 0)
+        stop=flight.t_final,          # end time in seconds (default: t_final)
+        time_step=0.05,               # seconds per frame (default: 0.1)
+    )
+
+    # Provide your own 3D model (any STL file)
+    flight.plots.animate_trajectory(
+        file_name="my_rocket.stl",
+        start=0.0,
+        stop=flight.t_final,
+        time_step=0.05,
+    )
+
+**animate_rotate — attitude-only animation**
+
+Useful for inspecting roll, pitch, and yaw behaviour without the distraction of
+the trajectory translation.  The rocket mesh is fixed at its position at
+``start`` and only rotated according to the quaternion solution.
+
+.. code-block:: python
+
+    flight.plots.animate_rotate(
+        start=0.0,
+        stop=flight.t_final,
+        time_step=0.05,
+    )
+
+**Parameters**
+
+Both methods share the same signature:
+
+.. list-table::
+   :header-rows: 1
+   :widths: 20 15 65
+
+   * - Parameter
+     - Default
+     - Description
+   * - ``file_name``
+     - ``None``
+     - Path to a ``.stl`` model file.  When ``None``, the built-in default
+       rocket shape packaged with RocketPy is used.
+   * - ``start``
+     - ``0``
+     - Animation start time in seconds.  Must be within
+       ``[0, flight.t_final]``.
+   * - ``stop``
+     - ``None``
+     - Animation end time in seconds.  ``None`` defaults to
+       ``flight.t_final``.
+   * - ``time_step``
+     - ``0.1``
+     - Duration of each frame in seconds.  Smaller values produce smoother
+       animations at the cost of longer render times.  Must be > 0.
+   * - ``**kwargs``
+     - —
+     - Additional keyword arguments forwarded to ``vedo.Plotter.show``
+       (e.g. ``viewup``, ``azimuth``, ``elevation``).
+
+**Tips**
+
+- A ``time_step`` of ``0.05`` (20 fps) is a good balance between smoothness
+  and performance for flights lasting tens of seconds.
+- Press **Escape** or close the vedo window to exit the animation loop early.
+- Both methods validate ``start``, ``stop``, ``time_step``, and the STL path
+  before any rendering begins, raising a :class:`ValueError` with a descriptive
+  message on invalid input.
+
 Forces and Moments
 ~~~~~~~~~~~~~~~~~~
 
diff --git a/docs/user/index.rst b/docs/user/index.rst
index 5afaee3a6..6f9d9effa 100644
--- a/docs/user/index.rst
+++ b/docs/user/index.rst
@@ -24,7 +24,10 @@ RocketPy's User Guide
    :caption: Special Case Simulations
 
    Compare Flights Class<compare_flights.rst>
+   Flight Comparator Class <flight_comparator.rst>
+   Parachute Triggers (Acceleration-Based) <parachute_triggers.rst>
    Deployable Payload <deployable.rst>
+   Controllers <controllers.rst>
    Air Brakes Example <airbrakes.rst>
    ../notebooks/sensors.ipynb
    ../matlab/matlab.rst
@@ -46,4 +49,6 @@ RocketPy's User Guide
    :caption: Further Analysis
 
    Function <function.rst>
-   Utilities <analysis.rst>
\ No newline at end of file
+   Utilities <analysis.rst>
+   Aerodynamic Surfaces <aerodynamics/surfaces.rst>
+   Logging <logging.rst>
diff --git a/docs/user/installation.rst b/docs/user/installation.rst
index 72ba1f42d..41ea2e3e4 100644
--- a/docs/user/installation.rst
+++ b/docs/user/installation.rst
@@ -19,7 +19,7 @@ If you want to choose a specific version to guarantee compatibility, you may ins
 
 .. code-block:: shell
 
-    pip install rocketpy==1.11.0
+    pip install rocketpy==1.13.0
 
 
 Optional Installation Method: ``conda``
@@ -138,22 +138,40 @@ To update Scipy and install netCDF4 using Conda, the following code is used:
 Optional Packages
 ^^^^^^^^^^^^^^^^^
 
-The EnvironmentAnalysis class requires a few extra packages to be installed.
-In case you want to use this class, you will need to install the following packages:
+RocketPy has several optional feature sets that can be installed individually.
 
-- `timezonefinder` : to allow for automatic timezone detection,
-- `windrose` : to allow for windrose plots,
-- `ipywidgets` : to allow for GIFs generation,
-- `jsonpickle` : to allow for saving and loading of class instances.
+**Environment Analysis** — extra plots and tools for the
+:class:`rocketpy.EnvironmentAnalysis` class:
 
-You can install all these packages by simply running the following lines in your preferred terminal:
+- `timezonefinder` : automatic timezone detection
+- `windrose` : windrose plots
+- `ipywidgets` : GIF generation
+- `jsonpickle` : saving and loading class instances
 
 .. code-block:: shell
 
     pip install rocketpy[env_analysis]
 
+**3D Flight Animation** — interactive 3D animations of rocket trajectory and
+attitude using `vedo <https://vedo.embl.es/>`_ (requires a desktop environment):
 
-Alternatively, you can instal all extra packages by running the following line in your preferred terminal:
+.. code-block:: shell
+
+    pip install rocketpy[animation]
+
+Once installed, you can render animations from a :class:`rocketpy.Flight` object:
+
+.. code-block:: python
+
+    # Animate rocket moving through 3D space
+    flight.plots.animate_trajectory(start=0, stop=flight.t_final, time_step=0.05)
+
+    # Animate attitude changes only (rocket stays centred)
+    flight.plots.animate_rotate(start=0, stop=flight.t_final, time_step=0.05)
+
+See :ref:`flightusage` for full details and parameter descriptions.
+
+**All extras** — install every optional dependency at once:
 
 .. code-block:: shell
 
diff --git a/docs/user/logging.rst b/docs/user/logging.rst
new file mode 100644
index 000000000..469175bde
--- /dev/null
+++ b/docs/user/logging.rst
@@ -0,0 +1,75 @@
+Logging
+=======
+
+RocketPy uses Python's built-in `logging <https://docs.python.org/3/library/logging.html>`_
+module to report internal runtime events, such as simulation progress,
+warnings and errors. By design, RocketPy is **silent by default**: unless
+you configure a handler, no log records are printed to the console. This
+follows the best practices recommended for Python libraries and keeps
+RocketPy from cluttering the output of applications that embed it.
+
+.. note::
+    This only affects internal runtime events. Output that you explicitly
+    request, such as ``flight.info()`` or ``rocket.all_info()``, continues
+    to print directly to the terminal regardless of the logging
+    configuration described here.
+
+Enabling logging
+-----------------
+
+The easiest way to see RocketPy's internal log messages is the
+:func:`rocketpy.utilities.enable_logging` helper, which attaches a console
+handler to RocketPy's logger hierarchy:
+
+.. jupyter-execute::
+
+    import rocketpy
+
+    rocketpy.utilities.enable_logging(level="INFO")
+
+Once enabled, operations such as saving a file or completing a simulation
+will emit messages to the console, for example:
+
+.. code-block:: text
+
+    INFO | rocketpy.simulation.flight | Simulation completed successfully.
+
+Log levels
+----------
+
+The ``level`` parameter controls the minimum severity of messages that are
+shown:
+
+- ``DEBUG``: high-frequency, low-level detail (e.g. solver iterations),
+  useful when troubleshooting a simulation.
+- ``INFO``: confirmations of completed operations (e.g. simulation
+  completed, file saved).
+- ``WARNING`` (default): unexpected but recoverable situations (e.g. a
+  missing motor, an automatically corrected geometry parameter).
+- ``ERROR``: a feature is broken or an optional dependency is missing.
+
+.. jupyter-execute::
+
+    # Show every internal runtime message, including solver ticks
+    rocketpy.utilities.enable_logging(level="DEBUG")
+
+Filtering by module
+--------------------
+
+Because each RocketPy module exposes its own logger (e.g.
+``rocketpy.simulation.flight``, ``rocketpy.environment.environment``), you
+can rely on the standard ``logging`` module to filter or redirect messages
+from specific modules, without using :func:`rocketpy.utilities.enable_logging`
+at all:
+
+.. code-block:: python
+
+    import logging
+
+    handler = logging.StreamHandler()
+    handler.setFormatter(logging.Formatter("%(levelname)s | %(name)s | %(message)s"))
+
+    # Only show logs coming from the Flight simulation module
+    flight_logger = logging.getLogger("rocketpy.simulation.flight")
+    flight_logger.addHandler(handler)
+    flight_logger.setLevel(logging.INFO)
diff --git a/docs/user/motors/motors.rst b/docs/user/motors/motors.rst
index b690cf9e8..2058ed677 100644
--- a/docs/user/motors/motors.rst
+++ b/docs/user/motors/motors.rst
@@ -33,6 +33,12 @@ Motors Usage
 
     Generic Motor Usage <genericmotor.rst>
 
+.. toctree::
+    :maxdepth: 3
+    :caption: Ring Cluster Motors
+
+    Ring Cluster Motor Usage <ringclustermotor.rst>
+
 .. toctree::
     :maxdepth: 3
     :caption: Tanks and Fluid
diff --git a/docs/user/motors/ringclustermotor.rst b/docs/user/motors/ringclustermotor.rst
new file mode 100644
index 000000000..07ec0842a
--- /dev/null
+++ b/docs/user/motors/ringclustermotor.rst
@@ -0,0 +1,93 @@
+.. _ringclustermotor:
+
+RingClusterMotor Class Usage
+============================
+
+Here we explore different features of the ``RingClusterMotor`` class.
+
+``RingClusterMotor`` models a ring (annular) configuration of ``N`` identical
+motors arranged symmetrically around a circular perimeter of a given radius,
+with no central motor along the rocket's longitudinal axis. It is a thin
+wrapper around a single, already-defined motor: all thrust-, mass- and
+inertia-related quantities are derived automatically from that base motor,
+its ``number`` of copies and their ``radius`` from the rocket's central axis.
+
+Key Assumptions
+---------------
+
+- ``number`` must be an integer ``>= 2``;
+- ``radius`` must be non-negative;
+- The base motor is currently expected to be a ``SolidMotor``, since
+  ``RingClusterMotor`` reuses its grain properties directly;
+- Motors are assumed identical and evenly spaced around the ring
+  (``360 / number`` degrees apart);
+- The transverse inertia (``I11``/``I22``) contribution of each motor is
+  computed explicitly via the parallel axis (Steiner) theorem for every
+  angular position, which keeps the result accurate even for the
+  asymmetric ``number=2`` case.
+
+Creating a Ring Cluster Motor
+------------------------------
+
+To define a ``RingClusterMotor``, we first need a fully defined base motor
+(typically a ``SolidMotor``), then wrap it with the number of motors in the
+cluster and their radial distance from the rocket's central axis:
+
+.. jupyter-execute::
+
+    from rocketpy import SolidMotor, RingClusterMotor
+
+    base_motor = SolidMotor(
+        thrust_source="../data/motors/cesaroni/Cesaroni_M1670.eng",
+        dry_mass=1.815,
+        dry_inertia=(0.125, 0.125, 0.002),
+        nozzle_radius=33 / 1000,
+        grain_number=5,
+        grain_density=1815,
+        grain_outer_radius=33 / 1000,
+        grain_initial_inner_radius=15 / 1000,
+        grain_initial_height=120 / 1000,
+        grain_separation=5 / 1000,
+        grains_center_of_mass_position=0.397,
+        center_of_dry_mass_position=0.317,
+        nozzle_position=0,
+        burn_time=3.9,
+        throat_radius=11 / 1000,
+        coordinate_system_orientation="nozzle_to_combustion_chamber",
+    )
+
+    cluster_motor = RingClusterMotor(
+        motor=base_motor,
+        number=4,
+        radius=0.1,
+    )
+
+    # Print the cluster (and underlying single-motor) information
+    cluster_motor.info()
+
+.. note::
+
+    ``RingClusterMotor`` does not read a thrust curve file directly. Instead,
+    it scales the ``thrust``, ``dry_mass``, ``propellant_mass`` and inertia
+    properties of the ``motor`` passed in by ``number``, so any changes to
+    ``base_motor`` must be made before it is wrapped.
+
+Since a ``RingClusterMotor`` is a ``Motor`` like any other, it can be attached
+to a ``Rocket`` with :meth:`Rocket.add_motor` exactly like a ``SolidMotor``,
+``HybridMotor`` or ``LiquidMotor`` would be.
+
+Visualizing the Cluster Layout
+-------------------------------
+
+The ``draw_cluster_layout`` method plots the position of each motor around
+the ring, which is useful to double-check the ``number`` and ``radius``
+parameters before running a simulation:
+
+.. jupyter-execute::
+
+    cluster_motor.draw_cluster_layout(rocket_radius=0.15)
+
+.. tip::
+
+    Passing ``rocket_radius`` draws the rocket's outer tube as a dashed
+    circle, which helps confirm that the motors fit inside the airframe.
diff --git a/docs/user/motors/tanks.rst b/docs/user/motors/tanks.rst
index 2c63cabaf..fe7da2fcb 100644
--- a/docs/user/motors/tanks.rst
+++ b/docs/user/motors/tanks.rst
@@ -104,7 +104,13 @@ The predefined ``CylindricalTank`` class is easy to use and is defined as such:
 
 .. jupyter-execute::
 
-  cylindrical_geometry = CylindricalTank(radius=0.1, height=2.0, spherical_caps=False)
+  cylindrical_geometry = CylindricalTank(radius_function=0.1, height=2.0, spherical_caps=False)
+
+.. deprecated:: 1.13.0
+  The ``radius`` keyword argument of ``CylindricalTank`` and ``SphericalTank``
+  has been renamed to ``radius_function``. Passing ``radius=`` still works but
+  now raises a ``DeprecationWarning`` and will be removed in v2.0.0. Use
+  ``radius_function=`` instead (it accepts the same constant radius value).
 
 .. note::
   The ``spherical_caps`` parameter is optional and defaults to ``False``. If set
@@ -116,7 +122,7 @@ The predefined ``SphericalTank`` is defined with:
 
 .. jupyter-execute::
 
-    spherical_geometry = SphericalTank(radius=0.1)
+    spherical_geometry = SphericalTank(radius_function=0.1)
 
 .. seealso::
   :class:`rocketpy.CylindricalTank` and :class:`rocketpy.SphericalTank`
diff --git a/docs/user/parachute_triggers.rst b/docs/user/parachute_triggers.rst
new file mode 100644
index 000000000..2799ea00d
--- /dev/null
+++ b/docs/user/parachute_triggers.rst
@@ -0,0 +1,279 @@
+Acceleration-Based Parachute Triggers
+======================================
+
+RocketPy lets parachute trigger functions access the state derivative
+``u_dot`` (which holds the accelerations at indices ``[3:6]``) in addition to
+pressure, height and the state vector. This enables avionics-style deployment
+logic that mimics how real flight computers use accelerometer (IMU) data to
+detect flight phases such as burnout, free-fall or liftoff.
+
+Overview
+--------
+
+Built-in string and numeric triggers rely on altitude and vertical velocity.
+By writing a **custom trigger function**, you can additionally use acceleration
+to implement mission-specific logic, for example:
+
+- Motor burnout detection (sudden drop in acceleration)
+- Apogee detection combining near-zero velocity with downward acceleration
+- Free-fall / ballistic coast detection (low total acceleration)
+- Liftoff detection (high total acceleration)
+
+For realistic noisy measurements, attach an :doc:`Accelerometer sensor
+</reference/classes/sensors/index>` to the rocket and read it inside the
+trigger instead of feeding the ideal ``u_dot`` directly.
+
+Trigger function signatures
+---------------------------
+
+A custom trigger callable may take **3, 4, or 5** arguments. RocketPy detects
+the signature automatically and only computes ``u_dot`` when a trigger asks for
+it (so legacy triggers pay no performance cost):
+
+- ``(pressure, height, state_vector)`` — the classic signature.
+- ``(pressure, height, state_vector, u_dot)`` — name the 4th argument
+  ``u_dot`` (or ``udot``/``acc``/``acceleration``) to receive the derivative;
+  any other name receives the ``sensors`` list instead.
+- ``(pressure, height, state_vector, sensors, u_dot)`` — receive both.
+
+``state_vector`` is ``[x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]`` and
+``u_dot`` is ``[vx, vy, vz, ax, ay, az, ...]``.
+
+Built-in apogee trigger
+-----------------------
+
+Deploys when the rocket starts descending (vertical velocity becomes negative):
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Main",
+        cd_s=10.0,
+        trigger="apogee",
+        sampling_rate=100,
+        lag=0.5,
+    )
+
+Numeric altitude trigger
+------------------------
+
+Pass a number to deploy at a fixed height above ground level while descending:
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Main",
+        cd_s=10.0,
+        trigger=400,  # meters above ground level
+        sampling_rate=100,
+        lag=0.5,
+    )
+
+Custom trigger: motor burnout
+-----------------------------
+
+Burnout is highly mission-dependent, so it is best expressed as a custom
+trigger with user-defined thresholds.
+
+Logic: detect a drop in vertical or total acceleration once the rocket is above
+a minimum height and still ascending.
+
+.. code-block:: python
+
+    def burnout_trigger_factory(
+        min_height=5.0,
+        min_vz=0.5,
+        az_threshold=-8.0,
+        total_acc_threshold=2.0,
+    ):
+        def burnout_trigger(_pressure, height, state_vector, u_dot):
+            ax, ay, az = u_dot[3], u_dot[4], u_dot[5]
+            total_acc = (ax**2 + ay**2 + az**2) ** 0.5
+            vz = state_vector[5]
+            if height < min_height or vz <= min_vz:
+                return False
+            return az < az_threshold or total_acc < total_acc_threshold
+
+        return burnout_trigger
+
+Attach it to a rocket:
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Drogue",
+        cd_s=1.0,
+        trigger=burnout_trigger_factory(
+            min_height=10.0,
+            min_vz=2.0,
+            az_threshold=-10.0,
+            total_acc_threshold=3.0,
+        ),
+        sampling_rate=100,
+        lag=1.5,
+    )
+
+Custom trigger: apogee by acceleration
+--------------------------------------
+
+Logic: near-zero vertical velocity together with downward acceleration.
+
+.. code-block:: python
+
+    def apogee_acc_trigger(_pressure, _height, state_vector, u_dot):
+        vz = state_vector[5]
+        az = u_dot[5]
+        return abs(vz) < 1.0 and az < -0.1
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Main",
+        cd_s=10.0,
+        trigger=apogee_acc_trigger,
+        sampling_rate=100,
+        lag=0.5,
+    )
+
+Custom trigger: free-fall
+-------------------------
+
+Logic: low total acceleration while descending above a small height.
+
+.. code-block:: python
+
+    def freefall_trigger(_pressure, height, state_vector, u_dot):
+        ax, ay, az = u_dot[3], u_dot[4], u_dot[5]
+        total_acc = (ax**2 + ay**2 + az**2) ** 0.5
+        vz = state_vector[5]
+        return height > 5.0 and vz < -0.2 and total_acc < 11.5
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Drogue",
+        cd_s=1.0,
+        trigger=freefall_trigger,
+        sampling_rate=100,
+        lag=1.5,
+    )
+
+Custom trigger: liftoff
+-----------------------
+
+Logic: detect motor ignition by high total acceleration.
+
+.. code-block:: python
+
+    def liftoff_trigger(_pressure, _height, _state_vector, u_dot):
+        ax, ay, az = u_dot[3], u_dot[4], u_dot[5]
+        total_acc = (ax**2 + ay**2 + az**2) ** 0.5
+        return total_acc > 15.0
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Lift",
+        cd_s=0.5,
+        trigger=liftoff_trigger,
+        sampling_rate=100,
+        lag=0.1,
+    )
+
+Custom trigger: using sensor measurements
+-----------------------------------------
+
+A 5-argument trigger receives both the ``sensors`` list and ``u_dot``, so you
+can cross-check a noisy accelerometer reading against the ideal derivative.
+
+.. code-block:: python
+
+    def advanced_trigger(_pressure, _height, _state_vector, sensors, u_dot):
+        if not sensors:
+            return False
+        acc_reading = sensors[0].measurement
+        if acc_reading is None or len(acc_reading) < 3:
+            return False
+        meas_az = acc_reading[2]
+        az = u_dot[5]
+        return az < -5.0 and meas_az < -5.0
+
+.. code-block:: python
+
+    rocket.add_parachute(
+        name="Advanced",
+        cd_s=1.5,
+        trigger=advanced_trigger,
+        sampling_rate=100,
+    )
+
+.. note::
+
+    For realistic IMU behavior, attach a RocketPy sensor with its own noise
+    model and read it inside the trigger via ``sensors``, instead of relying on
+    the ideal ``u_dot``. See the :doc:`Sensor Classes
+    </reference/classes/sensors/index>` for available sensors.
+
+Full example: dual deployment
+-----------------------------
+
+In RocketPy only one parachute is active at a time, so a dual-deploy avionics
+can be reproduced with two custom triggers — a drogue at burnout and a main at
+a lower altitude:
+
+.. code-block:: python
+
+    from rocketpy import Rocket, Flight, Environment
+
+    # Environment and rocket setup
+    env = Environment(latitude=32.99, longitude=-106.97, elevation=1400)
+    env.set_atmospheric_model(type="standard_atmosphere")
+
+    rocket = Rocket(...)  # configure your rocket (motor, fins, etc.)
+
+    # Drogue: deploy shortly after burnout (acceleration drop while ascending)
+    def drogue_burnout_trigger(_pressure, height, state_vector, u_dot):
+        az = u_dot[5]
+        vz = state_vector[5]
+        return height > 10 and vz > 1 and az < -8.0
+
+    rocket.add_parachute(
+        name="Drogue",
+        cd_s=1.0,
+        trigger=drogue_burnout_trigger,
+        sampling_rate=100,
+        lag=1.5,
+        noise=(0, 8.3, 0.5),  # pressure-signal noise
+    )
+
+    # Main: deploy below 800 m while descending
+    def main_deploy_trigger(_pressure, height, state_vector, u_dot):
+        vz = state_vector[5]
+        az = u_dot[5]
+        return height < 800 and vz < -5 and az > -15
+
+    rocket.add_parachute(
+        name="Main",
+        cd_s=10.0,
+        trigger=main_deploy_trigger,
+        sampling_rate=100,
+        lag=0.5,
+        noise=(0, 8.3, 0.5),
+    )
+
+    # Flight simulation
+    flight = Flight(
+        rocket=rocket,
+        environment=env,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+    )
+    flight.all_info()
+
+See Also
+--------
+
+- :doc:`Parachute Class Reference </reference/classes/Parachute>`
+- :doc:`Flight Simulation </user/flight>`
+- :doc:`Sensors </notebooks/sensors>`
diff --git a/docs/user/rocket/rocket_axes.rst b/docs/user/rocket/rocket_axes.rst
index 56fe17cad..aa99cb231 100644
--- a/docs/user/rocket/rocket_axes.rst
+++ b/docs/user/rocket/rocket_axes.rst
@@ -61,6 +61,8 @@ The following figure shows the two possibilities for the user input coordinate s
    the same as the **Body Axes Coordinate System**. The origin of the coordinate \
    system may still be different.
 
+.. _angular_position:
+
 Angular Position Inputs
 ~~~~~~~~~~~~~~~~~~~~~~~
 
diff --git a/docs/user/rocket/rocket_usage.rst b/docs/user/rocket/rocket_usage.rst
index 3496da6fd..5f8667694 100644
--- a/docs/user/rocket/rocket_usage.rst
+++ b/docs/user/rocket/rocket_usage.rst
@@ -290,12 +290,25 @@ Optionally, we can also define:
 - The parachute trigger system lag ``lag``.
 - The parachute trigger system noise ``noise``.
 
+.. note::
+
+    Since v1.13.0, :class:`~rocketpy.Parachute` is an **abstract base class**
+    and can no longer be instantiated directly. Instead, instantiate a concrete
+    parachute model such as :class:`~rocketpy.HemisphericalParachute` (used
+    below), which derives its geometry-dependent quantities (e.g. the added
+    mass during descent) from the parachute ``radius`` and ``height``. As a
+    convenience shortcut, ``Rocket.add_parachute(...)`` can still be called with
+    keyword arguments (``name``, ``cd_s``, ``trigger``, ...) and will build a
+    hemispherical parachute for you.
+
 Lets add two parachutes to the rocket, one that will be deployed at
 apogee and another that will be deployed at 800 meters above ground level:
 
 .. jupyter-execute::
 
-    main = calisto.add_parachute(
+    from rocketpy import HemisphericalParachute
+
+    main = HemisphericalParachute(
         name="Main",
         cd_s=10.0,
         trigger=800,
@@ -307,7 +320,7 @@ apogee and another that will be deployed at 800 meters above ground level:
         porosity=0.0432,
     )
 
-    drogue = calisto.add_parachute(
+    drogue = HemisphericalParachute(
         name="Drogue",
         cd_s=1.0,
         trigger="apogee",
@@ -318,6 +331,8 @@ apogee and another that will be deployed at 800 meters above ground level:
         height=1.5,
         porosity=0.0432,
     )
+    calisto.add_parachute(parachute = main)
+    calisto.add_parachute(parachute = drogue)
 
 .. seealso::
 
@@ -431,6 +446,18 @@ First, lets guarantee that the rocket is stable, by plotting the static margin:
     If it is unreasonably **high**, your rocket is **super stable** and the
     simulation will most likely **fail**.
 
+.. note::
+
+    RocketPy helps you catch this automatically: if the static margin is
+    **negative at motor ignition**, an
+    :class:`~rocketpy.exceptions.UnstableRocketWarning` is issued when the
+    rocket is used in a simulation. The check is skipped when the rocket has
+    any ``GenericSurface`` aerodynamic surfaces, since their lift coefficient
+    derivative is not accounted for in the center of pressure calculation,
+    which makes the static margin unreliable in that case. See
+    :doc:`/reference/classes/exceptions` for the full list of RocketPy
+    exceptions and warnings.
+
 The lets check all the information available about the rocket:
 
 .. jupyter-execute::
diff --git a/pyproject.toml b/pyproject.toml
index 4f1ecced4..35862cb9a 100644
--- a/pyproject.toml
+++ b/pyproject.toml
@@ -1,6 +1,6 @@
 [project]
 name = "rocketpy"
-version = "1.12.1"
+version = "1.13.0"
 description="Advanced 6-DOF trajectory simulation for High-Power Rocketry."
 dynamic = ["dependencies"]
 readme = "README.md"
@@ -34,6 +34,9 @@ build-backend = "setuptools.build_meta"
 [tool.setuptools]
 packages = { find = { where = ["."], include = ["rocketpy*"] } }
 
+[tool.setuptools.package-data]
+"rocketpy.plots" = ["assets/*.stl"]
+
 
 [tool.setuptools.dynamic]
 dependencies = { file = ["requirements.txt"] }
@@ -61,14 +64,18 @@ env-analysis = [
 ]
 
 monte-carlo = [
-    "imageio", 
+    "imageio",
     "multiprocess>=0.70",
     "statsmodels",
     "prettytable",
     "contextily>=1.0.0; python_version < '3.14'",
 ]
 
-all = ["rocketpy[env-analysis]", "rocketpy[monte-carlo]"]
+animation = [
+    "vedo>=2024.5.1"
+]
+
+all = ["rocketpy[env-analysis]", "rocketpy[monte-carlo]", "rocketpy[animation]"]
 
 
 [tool.coverage.report]
diff --git a/requirements-optional.txt b/requirements-optional.txt
index 58ed1030b..2961946ca 100644
--- a/requirements-optional.txt
+++ b/requirements-optional.txt
@@ -6,4 +6,5 @@ timezonefinder
 imageio
 multiprocess>=0.70
 statsmodels
-prettytable
\ No newline at end of file
+prettytable
+vedo>=2024.5.1
\ No newline at end of file
diff --git a/rocketpy/__init__.py b/rocketpy/__init__.py
index 852a16aef..05c800094 100644
--- a/rocketpy/__init__.py
+++ b/rocketpy/__init__.py
@@ -1,5 +1,10 @@
 from .control import _Controller
 from .environment import Environment, EnvironmentAnalysis
+from .exceptions import (
+    InvalidInertiaError,
+    InvalidParameterError,
+    UnstableRocketWarning,
+)
 from .mathutils import (
     Function,
     PiecewiseFunction,
@@ -18,6 +23,7 @@
     MassFlowRateBasedTank,
     Motor,
     PointMassMotor,
+    RingClusterMotor,
     SolidMotor,
     SphericalTank,
     Tank,
@@ -29,10 +35,14 @@
     AeroSurface,
     AirBrakes,
     Components,
+    EllipticalFin,
     EllipticalFins,
+    Fin,
     Fins,
+    FreeFormFin,
     FreeFormFins,
     GenericSurface,
+    HemisphericalParachute,
     LinearGenericSurface,
     NoseCone,
     Parachute,
@@ -40,6 +50,7 @@
     RailButtons,
     Rocket,
     Tail,
+    TrapezoidalFin,
     TrapezoidalFins,
 )
 from .sensitivity import SensitivityModel
@@ -58,3 +69,8 @@
     StochasticTail,
     StochasticTrapezoidalFins,
 )
+
+# Imported last: utilities pulls in Environment/Rocket/encoders, which are only
+# fully available once the imports above have run. Exposes
+# ``rocketpy.utilities`` (including ``enable_logging``) on ``import rocketpy``.
+from . import utilities
diff --git a/rocketpy/_encoders.py b/rocketpy/_encoders.py
index 58eeae809..669034636 100644
--- a/rocketpy/_encoders.py
+++ b/rocketpy/_encoders.py
@@ -1,6 +1,7 @@
 """Defines a custom JSON encoder for RocketPy objects."""
 
 import json
+import warnings
 from datetime import datetime
 from importlib import import_module
 
@@ -133,7 +134,13 @@ def object_hook(self, obj):
                     if hash_ is not None:
                         setattr(new_obj, "__rpy_hash", hash_)
                     return new_obj
-            except (ImportError, AttributeError):
+            except (ImportError, AttributeError) as exc:
+                warnings.warn(
+                    "Could not reconstruct a RocketPy object from the stored "
+                    f"signature {signature!r}: {exc}. Returning the raw data "
+                    "dictionary instead; the loaded object may be incomplete.",
+                    stacklevel=2,
+                )
                 return obj
         else:
             return obj
@@ -160,6 +167,7 @@ def set_minimal_flight_attributes(flight, obj):
         "apogee_time",
         "apogee",
         "parachute_events",
+        "parachutes_info",
         "impact_state",
         "impact_velocity",
         "x_impact",
@@ -238,10 +246,23 @@ def get_class_from_signature(signature):
     type
         Class defined by the signature.
     """
-    module = import_module(signature["module"])
+    module_name = signature["module"]
+    name = signature["name"]
+
+    # Backward compatibility: the parachute module was moved to the
+    # ``rocketpy.rocket.parachutes`` subpackage and the old concrete
+    # ``Parachute`` class became an abstract base, with the hemispherical model
+    # split out. Remap the legacy signature so ``.rpy`` files saved with older
+    # versions reconstruct as a concrete ``HemisphericalParachute`` instead of
+    # silently falling back to a raw dictionary.
+    if module_name == "rocketpy.rocket.parachute" and name == "Parachute":
+        module_name = "rocketpy.rocket.parachutes.hemispherical_parachute"
+        name = "HemisphericalParachute"
+
+    module = import_module(module_name)
     inner_class = None
 
-    for class_ in signature["name"].split("."):
+    for class_ in name.split("."):
         inner_class = getattr(module, class_)
 
     return inner_class
diff --git a/rocketpy/control/controller.py b/rocketpy/control/controller.py
index e81e70915..266389fa3 100644
--- a/rocketpy/control/controller.py
+++ b/rocketpy/control/controller.py
@@ -17,7 +17,7 @@ def __init__(
         self,
         interactive_objects,
         controller_function,
-        sampling_rate,
+        sampling_rate=None,
         initial_observed_variables=None,
         name="Controller",
     ):
@@ -38,16 +38,19 @@ def __init__(
             This function is expected to take the following arguments, in order:
 
             1. `time` (float): The current simulation time in seconds.
-            2. `sampling_rate` (float): The rate at which the controller
-               function is called, measured in Hertz (Hz).
+            2. `sampling_rate` (float or None): The rate at which the controller
+               function is called, measured in Hertz (Hz). It is None for
+               continuous controllers (called every solver step), so any
+               `1 / sampling_rate` computation must guard against None.
             3. `state` (list): The state vector of the simulation, structured as
                `[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]`.
             4. `state_history` (list): A record of the rocket's state at each
-               step throughout the simulation. The state_history is organized as
-               a list of lists, with each sublist containing a state vector. The
-               last item in the list always corresponds to the previous state
-               vector, providing a chronological sequence of the rocket's
-               evolving states.
+               step throughout the simulation. It is organized as a list of
+               lists, ordered oldest to newest, where each sublist is a
+               *time-prefixed* state row `[t, x, y, z, vx, vy, vz, e0, e1, e2,
+               e3, wx, wy, wz]` (i.e. the same layout as `Flight.solution`, one
+               leading `time` element ahead of the `state` layout in item 3).
+               The last item corresponds to the most recent recorded step.
             5. `observed_variables` (list): A list containing the variables that
                the controller function returns. The return of each controller
                function call is appended to the observed_variables list. The
@@ -71,12 +74,14 @@ def __init__(
             objects as needed. The function return statement can be used to save
             relevant information in the `observed_variables` list.
 
-            .. note:: The function will be called according to the sampling rate
-            specified.
-        sampling_rate : float
+            .. note:: The function will be called according to the sampling
+               rate specified. If `sampling_rate` is None, the controller
+               function is called at every solver step of the simulation.
+        sampling_rate : float, optional
             The sampling rate of the controller function in Hertz (Hz). This
             means that the controller function will be called every
-            `1/sampling_rate` seconds.
+            `1/sampling_rate` seconds. If None, it is treated as a
+            continuous controller and called at every solver step.
         initial_observed_variables : list, optional
             A list of the initial values of the variables that the controller
             function returns. This list is used to initialize the
@@ -178,10 +183,12 @@ def __call__(self, time, state_vector, state_history, sensors, environment):
 
             `[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]`.
         state_history : list
-            A list containing the state history of the simulation. The state
-            history is a list of every state vector of every step of the
-            simulation. The state history is a list of lists, where each
-            sublist is a state vector and is ordered from oldest to newest.
+            A list containing the state history of the simulation, ordered
+            oldest to newest. Each sublist is a *time-prefixed* state row
+            `[t, x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]` (the same
+            layout as `Flight.solution`, with a leading `time` element ahead of
+            the `state_vector` layout). The last item is the most recent
+            recorded step.
         sensors : list
             A list of sensors that are attached to the rocket. The most recent
             measurements of the sensors are provided with the
@@ -208,7 +215,15 @@ def __call__(self, time, state_vector, state_history, sensors, environment):
         if observed_variables is not None:
             self.observed_variables.append(observed_variables)
 
+    @property
+    def is_continuous(self):
+        """bool: True if the controller runs at every solver step (i.e.
+        ``sampling_rate`` is None), False if it is sampled at a fixed rate."""
+        return self.sampling_rate is None
+
     def __str__(self):
+        if self.is_continuous:
+            return f"Controller '{self.name}' with continuous sampling."
         return f"Controller '{self.name}' with sampling rate {self.sampling_rate} Hz."
 
     def info(self):
diff --git a/rocketpy/environment/environment.py b/rocketpy/environment/environment.py
index 8e379800c..d63f50c61 100644
--- a/rocketpy/environment/environment.py
+++ b/rocketpy/environment/environment.py
@@ -1,6 +1,7 @@
 # pylint: disable=too-many-public-methods, too-many-instance-attributes
 import bisect
 import json
+import logging
 import re
 import warnings
 from collections import namedtuple
@@ -11,10 +12,12 @@
 import pytz
 
 from rocketpy.environment.fetchers import (
+    fetch_aigfs_file_return_dataset,
     fetch_atmospheric_data_from_windy,
     fetch_gefs_ensemble,
     fetch_gfs_file_return_dataset,
     fetch_hiresw_file_return_dataset,
+    fetch_hrrr_file_return_dataset,
     fetch_nam_file_return_dataset,
     fetch_open_elevation,
     fetch_rap_file_return_dataset,
@@ -45,6 +48,8 @@
     geopotential_height_to_geometric_height,
 )
 
+logger = logging.getLogger(__name__)
+
 
 class Environment:
     """Keeps all environment information stored, such as wind and temperature
@@ -369,9 +374,11 @@ def __initialize_constants(self):
         self.__weather_model_map = WeatherModelMapping()
         self.__atm_type_file_to_function_map = {
             "forecast": {
+                "AIGFS": fetch_aigfs_file_return_dataset,
                 "GFS": fetch_gfs_file_return_dataset,
                 "NAM": fetch_nam_file_return_dataset,
                 "RAP": fetch_rap_file_return_dataset,
+                "HRRR": fetch_hrrr_file_return_dataset,
                 "HIRESW": fetch_hiresw_file_return_dataset,
             },
             "ensemble": {
@@ -533,20 +540,42 @@ def __set_wind_speed_function(self, source):
             interpolation="linear",
         )
 
+    def __set_wind_angle_function(self, source, attribute, output):
+        """Set ``attribute`` (e.g. ``wind_direction``) as a Function of height.
+        For 2D-array sources the angles are unwrapped across the 360/0 boundary
+        before linear interpolation, avoiding spurious spikes near the wrap."""
+        if isinstance(source, (np.ndarray, list, tuple)) and np.ndim(source) == 2:
+            array = np.asarray(source)
+            unwrapped_deg = np.rad2deg(np.unwrap(np.deg2rad(array[:, 1])))
+            unwrapped = Function(
+                np.column_stack((array[:, 0], unwrapped_deg)),
+                inputs="Height Above Sea Level (m)",
+                outputs=output,
+                interpolation="linear",
+            )
+            setattr(self, f"{attribute}_unwrapped", unwrapped)
+            source = Function(
+                lambda h: unwrapped(h) % 360,
+                inputs="Height Above Sea Level (m)",
+                outputs=output,
+            )
+        else:
+            source = Function(
+                source,
+                inputs="Height Above Sea Level (m)",
+                outputs=output,
+                interpolation="linear",
+            )
+        setattr(self, attribute, source)
+
     def __set_wind_direction_function(self, source):
-        self.wind_direction = Function(
-            source,
-            inputs="Height Above Sea Level (m)",
-            outputs="Wind Direction (Deg True)",
-            interpolation="linear",
+        self.__set_wind_angle_function(
+            source, "wind_direction", "Wind Direction (Deg True)"
         )
 
     def __set_wind_heading_function(self, source):
-        self.wind_heading = Function(
-            source,
-            inputs="Height Above Sea Level (m)",
-            outputs="Wind Heading (Deg True)",
-            interpolation="linear",
+        self.__set_wind_angle_function(
+            source, "wind_heading", "Wind Heading (Deg True)"
         )
 
     def __reset_barometric_height_function(self):
@@ -665,12 +694,13 @@ def __resolve_dictionary_for_dataset(self, dictionary, dataset):
     def __validate_dictionary(self, file, dictionary):
         # removed CMC until it is fixed.
         available_models = [
+            "AIGFS",
             "GFS",
             "NAM",
             "RAP",
+            "HRRR",
             "HIRESW",
             "GEFS",
-            "ERA5",
             "MERRA2",
         ]
         if isinstance(dictionary, str):
@@ -971,7 +1001,7 @@ def set_elevation(self, elevation="Open-Elevation"):
             self.elevation = elevation
         else:
             self.elevation = fetch_open_elevation(self.latitude, self.longitude)
-            print(f"Elevation received: {self.elevation} m")
+            logger.info("Elevation received: %.2f m", self.elevation)
 
     def set_topographic_profile(  # pylint: disable=redefined-builtin, unused-argument
         self, type, file, dictionary="netCDF4", crs=None
@@ -1010,14 +1040,13 @@ def set_topographic_profile(  # pylint: disable=redefined-builtin, unused-argume
                 # crsArray = nasa_dem.variables['crs'][:].tolist().
                 self.topographic_profile_activated = True
 
-                print("Region covered by the Topographical file: ")
-                print(
-                    f"Latitude from {self.elev_lat_array[-1]:.6f}° to "
-                    f"{self.elev_lat_array[0]:.6f}°"
-                )
-                print(
-                    f"Longitude from {self.elev_lon_array[0]:.6f}° to "
-                    f"{self.elev_lon_array[-1]:.6f}°"
+                logger.debug(
+                    "Topographical file coverage: lat [%.6f°, %.6f°], "
+                    "lon [%.6f°, %.6f°]",
+                    self.elev_lat_array[-1],
+                    self.elev_lat_array[0],
+                    self.elev_lon_array[0],
+                    self.elev_lon_array[-1],
                 )
 
     def get_elevation_from_topographic_profile(self, lat, lon):
@@ -1105,6 +1134,51 @@ def get_elevation_from_topographic_profile(self, lat, lon):
 
         return elevation
 
+    def __determine_pressure_conversion_factor(
+        self, pressure_conversion_factor, input_dict, input_file
+    ):
+        """Determine the numeric conversion factor (pressure -> Pa) based on
+        either the user's explicit input or auto-detection.
+
+        Parameters
+        ----------
+        pressure_conversion_factor : string, int, float or None
+            The user-supplied pressure conversion factor.
+        input_dict : string or None
+            The upper-case string name of the dictionary.
+        input_file : string or None
+            The upper-case string name of the file/model shortcut.
+
+        Returns
+        -------
+        conversion_factor : float, int or None
+            The numeric conversion factor to Pascal, or None if it needs to be
+            read from the file's units attribute.
+        """
+        if pressure_conversion_factor is not None:
+            # User explicitly supplied a value — honour it.
+            if isinstance(pressure_conversion_factor, str):
+                return (
+                    100 if pressure_conversion_factor.lower() in ("mbar", "hpa") else 1
+                )
+            return pressure_conversion_factor
+
+        # Auto-detect. Primary source: known-model lookup table.
+        # Fallback: units attribute inside the file.
+        # THREDDS (UCAR) models expose pressure on the 'isobaric' coordinate in
+        # Pa; NOMADS-GrADS models (GEFS, HIRESW) expose it on the 'lev'
+        # coordinate in hPa/millibars and must be scaled by 100.
+        _hpa_dicts = {"ECMWF", "ECMWF_V0", "MERRA2"}
+        _hpa_files = {"GEFS", "HIRESW"}
+        _pa_files = {"GFS", "NAM", "RAP", "HRRR", "AIGFS"}
+        if input_dict in _hpa_dicts or input_file in _hpa_dicts:
+            return 100
+        if input_file in _hpa_files:
+            return 100
+        if input_file in _pa_files:
+            return 1
+        return None
+
     def set_atmospheric_model(  # pylint: disable=too-many-statements
         self,
         type,  # pylint: disable=redefined-builtin
@@ -1114,6 +1188,7 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
         temperature=None,
         wind_u=0,
         wind_v=0,
+        pressure_conversion_factor=None,
     ):
         """Define the atmospheric model for this Environment.
 
@@ -1132,40 +1207,38 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
             - ``"windy"``: one of ``"ECMWF"``, ``"GFS"``, ``"ICON"`` or
               ``"ICONEU"``.
             - ``"forecast"``: local path, OPeNDAP URL, open
-              ``netCDF4.Dataset``, or one of ``"GFS"``, ``"NAM"`` or ``"RAP"``
-              for the latest available forecast.
+              ``netCDF4.Dataset``, or one of ``"AIGFS"``, ``"GFS"``,
+              ``"NAM"``, ``"RAP"``, ``"HRRR"`` or ``"HIRESW"`` for the
+              latest available forecast.
             - ``"reanalysis"``: local path, OPeNDAP URL, or open
               ``netCDF4.Dataset``.
             - ``"ensemble"``: local path, OPeNDAP URL, open
               ``netCDF4.Dataset``, or ``"GEFS"`` for the latest available
               forecast.
         dictionary : dict | str, optional
-            Variable-name mapping for ``"forecast"``, ``"reanalysis"`` and
-            ``"ensemble"``. It may be a custom dictionary or a built-in
-            mapping name (for example: ``"ECMWF"``, ``"ECMWF_v0"``,
-            ``"NOAA"``, ``"GFS"``, ``"NAM"``, ``"RAP"``, ``"HIRESW"``,
-            ``"GEFS"``, ``"MERRA2"`` or ``"CMC"``).
-
-            If ``dictionary`` is omitted and ``file`` is one of RocketPy's
-            latest-model shortcuts, the matching built-in mapping is selected
-            automatically. For ensemble datasets, the mapping must include the
-            ensemble dimension key (typically ``"ensemble"``).
-
+            A dictionary mapping variables in the netCDF4 file to standard
+            names. Meaning depends on ``type``:
+
+            - ``"standard_atmosphere"``, ``"custom_atmosphere"`` and
+              ``"wyoming_sounding"``: ignored.
+            - ``"windy"``: ignored.
+            - ``"forecast"``, ``"reanalysis"`` and ``"ensemble"``: local
+              dictionary, or one of the built-in mappings (e.g. ``"ECMWF"``,
+              ``"GFS"``, ``"MERRA2"``, ``"RAP"``, ``"HRRR"``, etc.) corresponding
+              to the file structure.
         pressure : float, string, array, callable, optional
-            This defines the atmospheric pressure profile.
-            Should be given if the type parameter is ``custom_atmosphere``. If not,
-            than the the ``Standard Atmosphere`` pressure will be used.
-            If a float is given, it will define a constant pressure
-            profile. The float should be in units of Pa.
-            If a string is given, it should point to a `.CSV` file
-            containing at most one header line and two columns of data.
-            The first column must be the geometric height above sea level in
-            meters while the second column must be the pressure in Pa.
-            If an array is given, it is expected to be a list or array
-            of coordinates (height in meters, pressure in Pa).
-            Finally, a callable or function is also accepted. The
-            function should take one argument, the height above sea
-            level in meters and return a corresponding pressure in Pa.
+            This defines the atmospheric pressure profile. Should be given if
+            the type parameter is ``custom_atmosphere``. If not, than the the
+            ``Standard Atmosphere`` pressure will be used. If a float is given,
+            it will define a constant pressure profile. The float should be in
+            units of Pa. If a string is given, it should point to a `.CSV` file
+            containing at most one header line and two columns of data. The first
+            column must be the geometric height above sea level in meters while
+            the second column must be the pressure in Pa. If an array is given,
+            it is expected to be a list or array of coordinates (height in
+            meters, pressure in Pa). Finally, a callable or function is also
+            accepted. The function should take one argument, the height above
+            sea level in meters and return a corresponding pressure in Pa.
         temperature : float, string, array, callable, optional
             This defines the atmospheric temperature profile. Should be given
             if the type parameter is ``custom_atmosphere``. If not, than the the
@@ -1208,6 +1281,16 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
             m/s). Finally, a callable or function is also accepted. The function
             should take one argument, the height above sea level in meters and
             return a corresponding wind-v in m/s.
+        pressure_conversion_factor : string, int, float, optional
+            This defines the pressure conversion factor to Pa when type is
+            ``forecast``, ``reanalysis``, or ``ensemble``. The pressure unit
+            from the data may not be in Pascal, so the correction is necessary.
+            Valid strings are ``"mbar"``, ``"hPa"``, or ``"Pa"``, or a strictly
+            positive number if using a custom pressure unit. If None (the default),
+            the conversion factor will be automatically detected based on the
+            model name (e.g. ERA5/ECMWF/MERRA2 reanalysis files commonly use hPa,
+            while online GFS/NAM/RAP/HRRR forecast models use Pa) or, if
+            unavailable, by reading the pressure unit attribute from the file.
 
         Returns
         -------
@@ -1257,6 +1340,35 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
             case "windy":
                 self.process_windy_atmosphere(file)
             case "forecast" | "reanalysis" | "ensemble":
+                # Capture the user-supplied names before __validate_dictionary
+                # converts them to dicts, so they can drive auto-detection.
+                _input_dict = (
+                    dictionary.upper() if isinstance(dictionary, str) else None
+                )
+                _input_file = file.upper() if isinstance(file, str) else None
+
+                # Validate format of user-supplied value (if any).
+                # When None, auto-detection runs after dictionary resolution.
+                if pressure_conversion_factor is not None:
+                    if not isinstance(pressure_conversion_factor, (float, int, str)):
+                        raise ValueError(
+                            "Argument 'pressure_conversion_factor' must be numeric or a standard pressure unit ('mbar', 'hPa', 'Pa')!"
+                        )
+                    if isinstance(pressure_conversion_factor, (float, int)):
+                        if pressure_conversion_factor <= 0:
+                            raise ValueError(
+                                "Argument 'pressure_conversion_factor' must be strictly positive!"
+                            )
+                    if isinstance(pressure_conversion_factor, str):
+                        if pressure_conversion_factor.lower() not in (
+                            "mbar",
+                            "hpa",
+                            "pa",
+                        ):
+                            raise ValueError(
+                                "Argument 'pressure_conversion_factor' unit must be a standard pressure unit ('mbar', 'hPa', 'Pa')!"
+                            )
+
                 if isinstance(file, str):
                     shortcut_map = self.__atm_type_file_to_function_map.get(type, {})
                     matching_shortcut = next(
@@ -1288,6 +1400,12 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
                         )
 
                 dictionary = self.__validate_dictionary(file, dictionary)
+
+                # Determine the numeric conversion factor (pressure → Pa).
+                conversion_factor = self.__determine_pressure_conversion_factor(
+                    pressure_conversion_factor, _input_dict, _input_file
+                )
+
                 try:
                     fetch_function = self.__atm_type_file_to_function_map[type][file]
                 except KeyError:
@@ -1297,9 +1415,35 @@ def set_atmospheric_model(  # pylint: disable=too-many-statements
                 dataset = fetch_function() if fetch_function is not None else file
 
                 if type in ["forecast", "reanalysis"]:
-                    self.process_forecast_reanalysis(dataset, dictionary)
+                    self.process_forecast_reanalysis(
+                        dataset, dictionary, conversion_factor=conversion_factor
+                    )
                 else:
-                    self.process_ensemble(dataset, dictionary)
+                    self.process_ensemble(dataset, dictionary, conversion_factor)
+
+                ground_pressure = self.pressure(self.elevation)
+                if not 30000 <= ground_pressure <= 120_000:
+                    if pressure_conversion_factor is None:
+                        hint = (
+                            "The unit was auto-detected from the file's pressure "
+                            "level variable or model name, but the result is still out of range. "
+                            "Override by passing pressure_conversion_factor explicitly "
+                            "('hPa' for ERA5/ECMWF/MERRA2 files, 'Pa' for online "
+                            "forecast models such as GFS, NAM, RAP, HRRR)."
+                        )
+                    else:
+                        hint = (
+                            f"pressure_conversion_factor='{pressure_conversion_factor}' "
+                            f"may be wrong. ERA5/ECMWF/MERRA2 reanalysis files store pressure "
+                            f"in hPa — use 'hPa'. Online forecast models "
+                            f"(GFS, NAM, RAP, HRRR) store pressure in Pa — use 'Pa'."
+                        )
+                    warnings.warn(
+                        f"Ground-level pressure is {ground_pressure:.0f} Pa, which is "
+                        f"outside the expected range [30 000 Pa, 120 000 Pa]. {hint}",
+                        UserWarning,
+                        stacklevel=2,
+                    )
             case _:  # pragma: no cover
                 raise ValueError(f"Unknown model type '{type}'.")
 
@@ -1610,11 +1754,11 @@ def process_wyoming_sounding(self, file):  # pylint: disable=too-many-statements
 
             Example:
 
-            http://weather.uwyo.edu/cgi-bin/sounding?region=samer&TYPE=TEXT%3ALIST&YEAR=2019&MONTH=02&FROM=0200&TO=0200&STNM=82599
+            https://weather.uwyo.edu/wsgi/sounding?datetime=2019-02-05%2012:00:00&id=83779&type=TEXT:LIST
 
         Notes
         -----
-        More can be found at: http://weather.uwyo.edu/upperair/sounding.html.
+        More can be found at: https://weather.uwyo.edu/upperair/sounding.shtml.
 
         Returns
         -------
@@ -1626,7 +1770,9 @@ def process_wyoming_sounding(self, file):  # pylint: disable=too-many-statements
         # Process Wyoming Sounding by finding data table and station info
         response_split_text = re.split("(<.{0,1}PRE>)", response.text)
         data_table = response_split_text[2]
-        station_info = response_split_text[6]
+        # Legacy CGI pages had extra <PRE> blocks with station information;
+        # current WSGI pages have a single block with the data table only.
+        station_info = response_split_text[6] if len(response_split_text) > 6 else None
 
         # Transform data table into np array
         data_array = []
@@ -1648,8 +1794,10 @@ def process_wyoming_sounding(self, file):  # pylint: disable=too-many-statements
         self.__set_temperature_function(data_array[:, (1, 2)])
 
         # Retrieve wind-u and wind-v from data array
-        ## Converts Knots to m/s
-        data_array[:, 7] = data_array[:, 7] * 1.852 / 3.6
+        ## Legacy pages report wind speed as SKNT (knots); current WSGI pages
+        ## report it as SPED (m/s) and need no conversion.
+        if "SKNT" in data_table.split("\n")[2]:
+            data_array[:, 7] = data_array[:, 7] * 1.852 / 3.6  # Knots to m/s
         ## Convert wind direction to wind heading
         data_array[:, 5] = (data_array[:, 6] + 180) % 360
         data_array[:, 3] = data_array[:, 7] * np.sin(data_array[:, 5] * np.pi / 180)
@@ -1667,18 +1815,21 @@ def process_wyoming_sounding(self, file):  # pylint: disable=too-many-statements
         self.__set_wind_direction_function(data_array[:, (1, 6)])
         self.__set_wind_speed_function(data_array[:, (1, 7)])
 
-        # Retrieve station elevation from station info
-        station_elevation_text = station_info.split("\n")[6]
-
-        # Convert station elevation text into float value
-        self.elevation = float(
-            re.findall(r"[0-9]+\.[0-9]+|[0-9]+", station_elevation_text)[0]
-        )
+        # Retrieve station elevation
+        if station_info is not None:
+            # Legacy pages: read it from the station information block
+            station_elevation_text = station_info.split("\n")[6]
+            self.elevation = float(
+                re.findall(r"[0-9]+\.[0-9]+|[0-9]+", station_elevation_text)[0]
+            )
+        else:
+            # Current WSGI pages: use the surface (first) level height
+            self.elevation = float(data_array[0, 1])
 
         # Save maximum expected height
         self._max_expected_height = data_array[-1, 1]
 
-    def process_forecast_reanalysis(self, file, dictionary):  # pylint: disable=too-many-locals,too-many-statements
+    def process_forecast_reanalysis(self, file, dictionary, conversion_factor):  # pylint: disable=too-many-locals,too-many-statements
         """Import and process atmospheric data from weather forecasts
         and reanalysis given as ``netCDF`` or ``OPeNDAP`` files.
         Sets pressure, temperature, wind-u and wind-v
@@ -1730,6 +1881,9 @@ def process_forecast_reanalysis(self, file, dictionary):  # pylint: disable=too-
                     "u_wind": "ugrdprs",
                     "v_wind": "vgrdprs",
                 }
+        conversion_factor : float, int
+            Specifies the factor by which the pressure will be multiplied
+            in order to transform it to Pascal.
 
         Returns
         -------
@@ -1761,13 +1915,17 @@ def process_forecast_reanalysis(self, file, dictionary):  # pylint: disable=too-
         # Some THREDDS datasets use projected x/y coordinates.
         if dictionary.get("projection") is not None:
             projection_variable = data.variables[dictionary["projection"]]
-            x_units = getattr(lon_array, "units", "m")
-            target_lon, target_lat = geodesic_to_lambert_conformal(
-                self.latitude,
-                self.longitude,
-                projection_variable,
-                x_units=x_units,
-            )
+            if dictionary.get("projection") == "LambertConformal_Projection":
+                x_units = getattr(lon_array, "units", "m")
+                target_lon, target_lat = geodesic_to_lambert_conformal(
+                    self.latitude,
+                    self.longitude,
+                    projection_variable,
+                    x_units=x_units,
+                )
+            else:
+                target_lon = self.longitude
+                target_lat = self.latitude
         else:
             target_lon = self.longitude
             target_lat = self.latitude
@@ -1778,7 +1936,7 @@ def process_forecast_reanalysis(self, file, dictionary):  # pylint: disable=too-
         _, lat_index = find_latitude_index(target_lat, lat_array)
 
         # Get pressure level data from file
-        levels = get_pressure_levels_from_file(data, dictionary)
+        levels = get_pressure_levels_from_file(data, dictionary, conversion_factor)
 
         # Get geopotential data from file
         try:
@@ -1979,7 +2137,7 @@ def process_forecast_reanalysis(self, file, dictionary):  # pylint: disable=too-
         # Close weather data
         data.close()
 
-    def process_ensemble(self, file, dictionary):  # pylint: disable=too-many-locals,too-many-statements
+    def process_ensemble(self, file, dictionary, conversion_factor):  # pylint: disable=too-many-locals,too-many-statements
         """Import and process atmospheric data from weather ensembles
         given as ``netCDF`` or ``OPeNDAP`` files. Sets pressure, temperature,
         wind-u and wind-v profiles and surface elevation obtained from a weather
@@ -2030,6 +2188,9 @@ def process_ensemble(self, file, dictionary):  # pylint: disable=too-many-locals
                     "u_wind": "ugrdprs",
                     "v_wind": "vgrdprs",
                 }
+        conversion_factor : float, int
+            Specifies the factor by which the pressure will be multiplied
+            in order to transform it to Pascal.
 
         See also
         --------
@@ -2065,13 +2226,17 @@ class for some dictionary examples.
         # coordinate system before locating the nearest grid cell.
         if dictionary.get("projection") is not None:
             projection_variable = data.variables[dictionary["projection"]]
-            x_units = getattr(lon_array, "units", "m")
-            target_lon, target_lat = geodesic_to_lambert_conformal(
-                self.latitude,
-                self.longitude,
-                projection_variable,
-                x_units=x_units,
-            )
+            if dictionary.get("projection") == "LambertConformal_Projection":
+                x_units = getattr(lon_array, "units", "m")
+                target_lon, target_lat = geodesic_to_lambert_conformal(
+                    self.latitude,
+                    self.longitude,
+                    projection_variable,
+                    x_units=x_units,
+                )
+            else:
+                target_lon = self.longitude
+                target_lat = self.latitude
         else:
             target_lon = self.longitude
             target_lat = self.latitude
@@ -2090,7 +2255,7 @@ class for some dictionary examples.
             num_members = 1
 
         # Get pressure level data from file
-        levels = get_pressure_levels_from_file(data, dictionary)
+        levels = get_pressure_levels_from_file(data, dictionary, conversion_factor)
 
         inverse_dictionary = {v: k for k, v in dictionary.items()}
         param_dictionary = {
@@ -2609,9 +2774,10 @@ def export_environment(self, filename="environment"):
 
         with open(filename + ".json", "w") as f:
             json.dump(export_env_dictionary, f, sort_keys=False, indent=4, default=str)
-        print(
-            f"Your Environment file was saved at '{filename}.json'. You can use "
-            "it in the future by using the custom_atmosphere atmospheric model."
+        logger.info(
+            "Your Environment file was saved at '%s.json'. "
+            "You can use it in the future by using the custom_atmosphere atmospheric model.",
+            filename,
         )
 
     def set_earth_geometry(self, datum):
@@ -2844,6 +3010,6 @@ def from_dict(cls, data):  # pylint: disable=too-many-statements
 
     results = doctest.testmod()
     if results.failed < 1:
-        print(f"All the {results.attempted} tests passed!")
+        logger.debug("All the %d tests passed!", results.attempted)
     else:
-        print(f"{results.failed} out of {results.attempted} tests failed.")
+        logger.error("%d out of %d tests failed.", results.failed, results.attempted)
diff --git a/rocketpy/environment/environment_analysis.py b/rocketpy/environment/environment_analysis.py
index 13589078e..e4dcbd021 100644
--- a/rocketpy/environment/environment_analysis.py
+++ b/rocketpy/environment/environment_analysis.py
@@ -2,6 +2,7 @@
 import copy
 import datetime
 import json
+import logging
 import warnings
 from collections import defaultdict
 from functools import cached_property
@@ -24,6 +25,8 @@
 from ..units import convert_units
 from .environment import Environment
 
+logger = logging.getLogger(__name__)
+
 # TODO: the average_wind_speed_profile_by_hour and similar methods could be more abstract than currently are
 
 
@@ -236,13 +239,15 @@ def __check_requirements(self):
                 check_requirement_version(module_name, version)
             except (ValueError, ImportError) as e:
                 has_error = True
-                print(
-                    f"The following error occurred while importing {module_name}: {e}"
+                logger.error(
+                    "The following error occurred while importing %s: %s",
+                    module_name,
+                    e,
                 )
         if has_error:
-            print(
+            logger.error(
                 "Given the above errors, some methods may not work. Please run "
-                + "'pip install rocketpy[env_analysis]' to install extra requirements."
+                "'pip install rocketpy[env_analysis]' to install extra requirements."
             )
 
     def __init_surface_dictionary(self):
@@ -460,8 +465,6 @@ def __init_data_parsing_units(self):
             "height_ASL": "m",
             "pressure": "hPa",
             "temperature": "K",
-            "wind_direction": "deg",
-            "wind_heading": "deg",
             "wind_speed": "m/s",
             "wind_velocity_x": "m/s",
             "wind_velocity_y": "m/s",
@@ -508,8 +511,9 @@ def __init_unit_system(self):
             }
         else:
             # Default to SI
-            print(
-                f"Defaulting to SI unit system, the {self.unit_system_string} was not found."
+            logger.warning(
+                "Defaulting to SI unit system, the '%s' unit system was not found.",
+                self.unit_system_string,
             )
             self.unit_system = {
                 "length": "m",
@@ -570,8 +574,6 @@ def __parse_pressure_level_data(self):
         Must compute the following for each date and hour available in the dataset:
         - pressure = Function(..., inputs="Height Above Ground Level (m)", outputs="Pressure (Pa)")
         - temperature = Function(..., inputs="Height Above Ground Level (m)", outputs="Temperature (K)")
-        - wind_direction = Function(..., inputs="Height Above Ground Level (m)", outputs="Wind Direction (Deg True)")
-        - wind_heading = Function(..., inputs="Height Above Ground Level (m)", outputs="Wind Heading (Deg True)")
         - wind_speed = Function(..., inputs="Height Above Ground Level (m)", outputs="Wind Speed (m/s)")
         - wind_velocity_x = Function(..., inputs="Height Above Ground Level (m)", outputs="Wind Velocity X (m/s)")
         - wind_velocity_y = Function(..., inputs="Height Above Ground Level (m)", outputs="Wind Velocity Y (m/s)")
@@ -722,39 +724,6 @@ def __parse_pressure_level_data(self):
             )
             dictionary[date_string][hour_string]["wind_speed"] = wind_speed_function
 
-            # Create function for wind heading levels
-            wind_heading_array = (
-                np.arctan2(wind_velocity_x_array, wind_velocity_y_array)
-                * (180 / np.pi)
-                % 360
-            )
-
-            wind_heading_points_array = np.array(
-                [height_above_ground_level_array, wind_heading_array]
-            ).T
-            wind_heading_function = Function(
-                wind_heading_points_array,
-                inputs="Height Above Ground Level (m)",
-                outputs="Wind Heading (Deg True)",
-                extrapolation="constant",
-            )
-            dictionary[date_string][hour_string]["wind_heading"] = wind_heading_function
-
-            # Create function for wind direction levels
-            wind_direction_array = (wind_heading_array - 180) % 360
-            wind_direction_points_array = np.array(
-                [height_above_ground_level_array, wind_direction_array]
-            ).T
-            wind_direction_function = Function(
-                wind_direction_points_array,
-                inputs="Height Above Ground Level (m)",
-                outputs="Wind Direction (Deg True)",
-                extrapolation="constant",
-            )
-            dictionary[date_string][hour_string]["wind_direction"] = (
-                wind_direction_function
-            )
-
         return (dictionary, lat0, lat1, lon0, lon1)
 
     @property
@@ -985,8 +954,6 @@ def converted_pressure_level_data(self):
         conversion_dict = {
             "pressure": self.unit_system["pressure"],
             "temperature": self.unit_system["temperature"],
-            "wind_direction": self.unit_system["angle"],
-            "wind_heading": self.unit_system["angle"],
             "wind_speed": self.unit_system["wind_speed"],
             "wind_velocity_x": self.unit_system["wind_speed"],
             "wind_velocity_y": self.unit_system["wind_speed"],
@@ -2843,9 +2810,10 @@ def export_mean_profiles(self, filename="export_env_analysis"):
                     self.export_dictionary, sort_keys=False, indent=4, default=str
                 )
             )
-        print(
-            f"Your Environment Analysis file was saved, check it out: {filename}.json\n"
-            "You can use it to set a `customAtmosphere` atmospheric model"
+        logger.info(
+            "Your Environment Analysis file was saved: %s.json. "
+            "You can use it to set a customAtmosphere atmospheric model.",
+            filename,
         )
 
     @classmethod
@@ -2884,7 +2852,7 @@ def save(self, filename="env_analysis_dict"):
         file = open(filename, "w")  # pylint: disable=consider-using-with
         file.write(encoded_class)
         file.close()
-        print("Your Environment Analysis file was saved, check it out: " + filename)
+        logger.info("Your Environment Analysis file was saved: %s", filename)
 
     def create_environment_object(
         self, gravity=None, date=None, datum="SIRGAS2000", max_expected_height=80000.0
diff --git a/rocketpy/environment/fetchers.py b/rocketpy/environment/fetchers.py
index de63d53ad..740e9818a 100644
--- a/rocketpy/environment/fetchers.py
+++ b/rocketpy/environment/fetchers.py
@@ -3,6 +3,7 @@
 functions may be changed without notice in future feature releases.
 """
 
+import logging
 import re
 import time
 from datetime import datetime, timedelta, timezone
@@ -12,6 +13,8 @@
 
 from rocketpy.tools import exponential_backoff
 
+logger = logging.getLogger(__name__)
+
 MAX_RETRY_DELAY_SECONDS = 600
 
 
@@ -37,7 +40,9 @@ def fetch_open_elevation(lat, lon):
     RuntimeError
         If there is a problem reaching the Open-Elevation API servers.
     """
-    print(f"Fetching elevation from open-elevation.com for lat={lat}, lon={lon}...")
+    logger.debug(
+        "Fetching elevation from open-elevation.com for lat=%s, lon=%s", lat, lon
+    )
     request_url = f"https://api.open-elevation.com/api/v1/lookup?locations={lat},{lon}"
     try:
         response = requests.get(request_url)
@@ -195,6 +200,78 @@ def fetch_rap_file_return_dataset(max_attempts=10, base_delay=2):
     raise RuntimeError("Unable to load latest weather data for RAP through " + file_url)
 
 
+def fetch_hrrr_file_return_dataset(max_attempts=10, base_delay=2):
+    """Fetches the latest HRRR (High-Resolution Rapid Refresh) dataset from
+    the NOAA's GrADS data server using the OpenDAP protocol.
+
+    Parameters
+    ----------
+    max_attempts : int, optional
+        The maximum number of attempts to fetch the dataset. Default is 10.
+    base_delay : int, optional
+        The base delay in seconds between attempts. Default is 2.
+
+    Returns
+    -------
+    netCDF4.Dataset
+        The HRRR dataset.
+
+    Raises
+    ------
+    RuntimeError
+        If unable to load the latest weather data for HRRR.
+    """
+    file_url = "https://thredds.ucar.edu/thredds/dodsC/grib/NCEP/HRRR/CONUS_2p5km/Best"
+    attempt_count = 0
+    while attempt_count < max_attempts:
+        try:
+            return netCDF4.Dataset(file_url)
+        except OSError:
+            attempt_count += 1
+            time.sleep(min(base_delay**attempt_count, MAX_RETRY_DELAY_SECONDS))
+
+    raise RuntimeError(
+        "Unable to load latest weather data for HRRR through " + file_url
+    )
+
+
+def fetch_aigfs_file_return_dataset(max_attempts=10, base_delay=2):
+    """Fetches the latest AIGFS (Artificial Intelligence GFS) dataset from
+    the NOAA's GrADS data server using the OpenDAP protocol.
+
+    Parameters
+    ----------
+    max_attempts : int, optional
+        The maximum number of attempts to fetch the dataset. Default is 10.
+    base_delay : int, optional
+        The base delay in seconds between attempts. Default is 2.
+
+    Returns
+    -------
+    netCDF4.Dataset
+        The AIGFS dataset.
+
+    Raises
+    ------
+    RuntimeError
+        If unable to load the latest weather data for AIGFS.
+    """
+    file_url = (
+        "https://thredds.ucar.edu/thredds/dodsC/grib/NCEP/AIGFS/Global_0p25deg/Best"
+    )
+    attempt_count = 0
+    while attempt_count < max_attempts:
+        try:
+            return netCDF4.Dataset(file_url)
+        except OSError:
+            attempt_count += 1
+            time.sleep(min(base_delay**attempt_count, MAX_RETRY_DELAY_SECONDS))
+
+    raise RuntimeError(
+        "Unable to load latest weather data for AIGFS through " + file_url
+    )
+
+
 def fetch_hiresw_file_return_dataset(max_attempts=10, base_delay=2):
     """Fetches the latest HiResW (High-Resolution Window) dataset from the NOAA's
     GrADS data server using the OpenDAP protocol.
diff --git a/rocketpy/environment/tools.py b/rocketpy/environment/tools.py
index 4a06ef2c4..5e23de0f9 100644
--- a/rocketpy/environment/tools.py
+++ b/rocketpy/environment/tools.py
@@ -5,6 +5,7 @@
 future to improve their performance and usability.
 """
 
+import logging
 import math
 import warnings
 
@@ -13,6 +14,8 @@
 
 from rocketpy.tools import bilinear_interpolation
 
+logger = logging.getLogger(__name__)
+
 ## Wind data functions
 
 
@@ -169,7 +172,7 @@ def geodesic_to_lambert_conformal(lat, lon, projection_variable, x_units="m"):
 ## These functions are meant to be used with netcdf4 datasets
 
 
-def get_pressure_levels_from_file(data, dictionary):
+def get_pressure_levels_from_file(data, dictionary, conversion_factor):
     """Extracts pressure levels from a netCDF4 dataset and converts them to Pa.
 
     Parameters
@@ -178,6 +181,11 @@ def get_pressure_levels_from_file(data, dictionary):
         The netCDF4 dataset containing the pressure level data.
     dictionary : dict
         A dictionary mapping variable names to dataset keys.
+    conversion_factor : float, int, or None
+        Specifies the factor by which the pressure will be multiplied to
+        transform it to Pascal. If ``None``, the factor is auto-detected from
+        the ``units`` attribute of the pressure level variable in the dataset
+        (e.g. ``"millibars"`` or ``"hPa"`` → 100; ``"Pa"`` → 1).
 
     Returns
     -------
@@ -190,8 +198,14 @@ def get_pressure_levels_from_file(data, dictionary):
         If the pressure levels cannot be read from the file.
     """
     try:
-        # Convert mbar to Pa
-        levels = 100 * data.variables[dictionary["level"]][:]
+        level_var = data.variables[dictionary["level"]]
+        if conversion_factor is None:
+            raw_units = getattr(level_var, "units", "").lower().strip()
+            if raw_units in ("hpa", "mbar", "millibars", "hectopascal", "hectopascals"):
+                conversion_factor = 100
+            else:
+                conversion_factor = 1
+        levels = conversion_factor * level_var[:]
     except KeyError as e:
         raise ValueError(
             "Unable to read pressure levels from file. Check file and dictionary."
@@ -839,6 +853,6 @@ def utm_to_geodesic(  # pylint: disable=too-many-locals,too-many-statements
 
     results = doctest.testmod()
     if results.failed < 1:
-        print(f"All the {results.attempted} tests passed!")
+        logger.info("All the %d tests passed!", results.attempted)
     else:
-        print(f"{results.failed} out of {results.attempted} tests failed.")
+        logger.error("%d out of %d tests failed.", results.failed, results.attempted)
diff --git a/rocketpy/environment/weather_model_mapping.py b/rocketpy/environment/weather_model_mapping.py
index b054a35c4..c8617a523 100644
--- a/rocketpy/environment/weather_model_mapping.py
+++ b/rocketpy/environment/weather_model_mapping.py
@@ -48,11 +48,11 @@ class WeatherModelMapping:
         "u_wind": "ugrdprs",
         "v_wind": "vgrdprs",
     }
-    NAM = {
+    AIGFS = {
         "time": "time",
-        "latitude": "y",
-        "longitude": "x",
-        "projection": "LambertConformal_Projection",
+        "latitude": "lat",
+        "longitude": "lon",
+        "projection": "LatLon_Projection",
         "level": "isobaric",
         "temperature": "Temperature_isobaric",
         "surface_geopotential_height": None,
@@ -73,6 +73,19 @@ class WeatherModelMapping:
         "u_wind": "ugrdprs",
         "v_wind": "vgrdprs",
     }
+    NAM = {
+        "time": "time",
+        "latitude": "y",
+        "longitude": "x",
+        "projection": "LambertConformal_Projection",
+        "level": "isobaric",
+        "temperature": "Temperature_isobaric",
+        "surface_geopotential_height": None,
+        "geopotential_height": "Geopotential_height_isobaric",
+        "geopotential": None,
+        "u_wind": "u-component_of_wind_isobaric",
+        "v_wind": "v-component_of_wind_isobaric",
+    }
     ECMWF_v0 = {
         "time": "time",
         "latitude": "latitude",
@@ -148,20 +161,20 @@ class WeatherModelMapping:
         "u_wind": "ugrdprs",
         "v_wind": "vgrdprs",
     }
-    CMC = {
+    HRRR = {
         "time": "time",
-        "latitude": "lat",
-        "longitude": "lon",
-        "level": "lev",
-        "ensemble": "ens",
-        "temperature": "tmpprs",
+        "latitude": "y",
+        "longitude": "x",
+        "projection": "LambertConformal_Projection",
+        "level": "isobaric",
+        "temperature": "Temperature_isobaric",
         "surface_geopotential_height": None,
-        "geopotential_height": "hgtprs",
+        "geopotential_height": "Geopotential_height_isobaric",
         "geopotential": None,
-        "u_wind": "ugrdprs",
-        "v_wind": "vgrdprs",
+        "u_wind": "u-component_of_wind_isobaric",
+        "v_wind": "v-component_of_wind_isobaric",
     }
-    CMC_LEGACY = {
+    CMC = {
         "time": "time",
         "latitude": "lat",
         "longitude": "lon",
@@ -211,17 +224,6 @@ class WeatherModelMapping:
         "u_wind": "ugrdprs",
         "v_wind": "vgrdprs",
     }
-    HIRESW_LEGACY = {
-        "time": "time",
-        "latitude": "lat",
-        "longitude": "lon",
-        "level": "lev",
-        "temperature": "tmpprs",
-        "surface_geopotential_height": "hgtsfc",
-        "geopotential_height": "hgtprs",
-        "u_wind": "ugrdprs",
-        "v_wind": "vgrdprs",
-    }
     MERRA2 = {
         "time": "time",
         "latitude": "lat",
@@ -235,19 +237,6 @@ class WeatherModelMapping:
         "u_wind": "U",
         "v_wind": "V",
     }
-    MERRA2_LEGACY = {
-        "time": "time",
-        "latitude": "lat",
-        "longitude": "lon",
-        "level": "lev",
-        "temperature": "T",
-        "surface_geopotential_height": None,
-        "surface_geopotential": "PHIS",
-        "geopotential_height": "H",
-        "geopotential": None,
-        "u_wind": "U",
-        "v_wind": "V",
-    }
 
     def __init__(self):
         """Build the lookup table with default and legacy mapping aliases."""
@@ -255,6 +244,7 @@ def __init__(self):
         self.all_dictionaries = {
             "GFS": self.GFS,
             "GFS_LEGACY": self.GFS_LEGACY,
+            "AIGFS": self.AIGFS,
             "NAM": self.NAM,
             "NAM_LEGACY": self.NAM_LEGACY,
             "ECMWF_v0": self.ECMWF_v0,
@@ -263,14 +253,12 @@ def __init__(self):
             "NOAA_LEGACY": self.NOAA_LEGACY,
             "RAP": self.RAP,
             "RAP_LEGACY": self.RAP_LEGACY,
+            "HRRR": self.HRRR,
             "CMC": self.CMC,
-            "CMC_LEGACY": self.CMC_LEGACY,
             "GEFS": self.GEFS,
             "GEFS_LEGACY": self.GEFS_LEGACY,
             "HIRESW": self.HIRESW,
-            "HIRESW_LEGACY": self.HIRESW_LEGACY,
             "MERRA2": self.MERRA2,
-            "MERRA2_LEGACY": self.MERRA2_LEGACY,
         }
 
     def get(self, model):
diff --git a/rocketpy/exceptions.py b/rocketpy/exceptions.py
new file mode 100644
index 000000000..e6bdc4355
--- /dev/null
+++ b/rocketpy/exceptions.py
@@ -0,0 +1,30 @@
+"""Custom exceptions and warnings for RocketPy."""
+
+# TODO: progressively adopt these custom exceptions across the codebase.
+# Many modules still ``raise ValueError``/``TypeError`` directly; migrate those
+# to the appropriate ``RocketPyError`` subclass (adding new exception types here
+# as needed) so users can reliably catch ``RocketPyError`` and its subclasses.
+
+
+class RocketPyError(Exception):
+    """Base class for all RocketPy exceptions."""
+
+
+class InvalidParameterError(RocketPyError, ValueError):
+    """Raised when a constructor parameter has an invalid value (e.g. negative
+    radius or mass)."""
+
+
+class InvalidInertiaError(RocketPyError, ValueError):
+    """Raised when the inertia tuple/list does not have the expected length."""
+
+
+class UnstableRocketWarning(UserWarning):
+    """Issued when the rocket's static margin is negative at motor ignition,
+    indicating an aerodynamically unstable configuration.
+
+    Not issued when the rocket has any ``GenericSurface`` aerodynamic
+    surfaces, since their lift coefficient derivative is not accounted for
+    in the center of pressure calculation, making the static margin
+    unreliable for this check in that case.
+    """
diff --git a/rocketpy/mathutils/function.py b/rocketpy/mathutils/function.py
index 33a82ec01..8148dd454 100644
--- a/rocketpy/mathutils/function.py
+++ b/rocketpy/mathutils/function.py
@@ -5,6 +5,7 @@
 carefully as it may impact all the rest of the project.
 """
 
+import logging
 import operator
 import warnings
 from bisect import bisect_left
@@ -25,10 +26,13 @@
     RBFInterpolator,
     RegularGridInterpolator,
 )
+from scipy.spatial import Delaunay  # pylint: disable=no-name-in-module
 
 from rocketpy.plots.plot_helpers import show_or_save_plot
 from rocketpy.tools import deprecated, from_hex_decode, to_hex_encode
 
+logger = logging.getLogger(__name__)
+
 NUMERICAL_TYPES = (float, int, complex, np.integer, np.floating)
 INTERPOLATION_TYPES = {
     "linear": 0,
@@ -519,7 +523,9 @@ def linear_interpolation(x, x_min, x_max, x_data, y_data, coeffs):  # pylint: di
                         return (x - x_left) * (dy / dx) + y_left
 
                 else:
-                    interpolator = LinearNDInterpolator(self._domain, self._image)
+                    tri = Delaunay(self._domain)
+                    interpolator = LinearNDInterpolator(tri, self._image)
+                    self._nd_triangulation = tri
 
                     def linear_interpolation(x, x_min, x_max, x_data, y_data, coeffs):  # pylint: disable=unused-argument
                         return interpolator(x)
@@ -827,8 +833,11 @@ def __get_value_opt_nd(self, *args):
         min_domain = self._domain.T.min(axis=1)
         max_domain = self._domain.T.max(axis=1)
 
-        lower, upper = args < min_domain, args > max_domain
-        extrap = np.logical_or(lower.any(axis=1), upper.any(axis=1))
+        if self.__interpolation__ == "linear" and hasattr(self, "_nd_triangulation"):
+            extrap = self._nd_triangulation.find_simplex(args) < 0
+        else:
+            lower, upper = args < min_domain, args > max_domain
+            extrap = np.logical_or(lower.any(axis=1), upper.any(axis=1))
 
         if extrap.any():
             result[extrap] = self._extrapolation_func(
@@ -2012,7 +2021,7 @@ def plot(self, *args, **kwargs):
             elif self.__dom_dim__ == 2:
                 self.plot_2d(*args, **kwargs)
             else:
-                print("Error: Only functions with 1D or 2D domains can be plotted.")
+                logger.error("Only functions with 1D or 2D domains can be plotted.")
 
     @deprecated(
         reason="The `Function.plot1D` method is set to be deprecated and fully "
@@ -4399,6 +4408,6 @@ def reset_funcified_methods(instance):
 
     results = doctest.testmod()
     if results.failed < 1:
-        print(f"All the {results.attempted} tests passed!")
+        logger.info("All the %d tests passed!", results.attempted)
     else:
-        print(f"{results.failed} out of {results.attempted} tests failed.")
+        logger.error("%d out of %d tests failed.", results.failed, results.attempted)
diff --git a/rocketpy/mathutils/vector_matrix.py b/rocketpy/mathutils/vector_matrix.py
index 9c8bde144..c40e01e4b 100644
--- a/rocketpy/mathutils/vector_matrix.py
+++ b/rocketpy/mathutils/vector_matrix.py
@@ -1,9 +1,12 @@
+import logging
 from cmath import isclose
 from functools import cached_property
 from itertools import product
 
 from rocketpy.tools import euler313_to_quaternions, normalize_quaternions
 
+logger = logging.getLogger(__name__)
+
 
 class Vector:
     """Pure python basic R3 vector class designed for simple operations.
@@ -1108,6 +1111,6 @@ def from_dict(cls, data):
 
     results = doctest.testmod()
     if results.failed < 1:
-        print(f"All the {results.attempted} tests passed!")
+        logger.info("All the %d tests passed!", results.attempted)
     else:
-        print(f"{results.failed} out of {results.attempted} tests failed.")
+        logger.error("%d out of %d tests failed.", results.failed, results.attempted)
diff --git a/rocketpy/motors/__init__.py b/rocketpy/motors/__init__.py
index b13ff9392..56f24dddf 100644
--- a/rocketpy/motors/__init__.py
+++ b/rocketpy/motors/__init__.py
@@ -4,6 +4,7 @@
 from .liquid_motor import LiquidMotor
 from .motor import GenericMotor, Motor
 from .point_mass_motor import PointMassMotor
+from .ring_cluster_motor import RingClusterMotor
 from .solid_motor import SolidMotor
 from .tank import (
     LevelBasedTank,
diff --git a/rocketpy/motors/ring_cluster_motor.py b/rocketpy/motors/ring_cluster_motor.py
new file mode 100644
index 000000000..af0d544c3
--- /dev/null
+++ b/rocketpy/motors/ring_cluster_motor.py
@@ -0,0 +1,368 @@
+# pylint: disable=invalid-name
+import matplotlib.pyplot as plt
+import numpy as np
+
+from ..mathutils.function import Function, funcify_method
+from ..tools import parallel_axis_theorem_from_com
+from .motor import Motor
+
+
+class RingClusterMotor(Motor):
+    """
+    A class representing a cluster of N identical motors arranged symmetrically.
+
+    This class models a ring (annular) cluster configuration where a specific
+    number of identical motors (N >= 2) are arranged symmetrically along a
+    circular perimeter of a given radius. Note that this model assumes no
+    central motor is present along the rocket's longitudinal axis. The total
+    inertia tensors (Ixx and Iyy) are computed by explicitly summing the
+    contribution of each individual motor based on its angular position,
+    ensuring mathematical accuracy for all configurations, including the
+    asymmetric transverse inertia case of N=2.
+
+    Attributes
+    ----------
+    motor : SolidMotor
+        The single motor instance used in the cluster.
+    number : int
+        The number of motors in the cluster.
+    radius : float
+        The radial distance from the rocket's central axis to the center of each motor.
+    """
+
+    def __init__(self, motor, number, radius):
+        """
+        Initialize the ClusterMotor.
+
+        Parameters
+        ----------
+        motor : SolidMotor
+            The base motor to be clustered.
+        number : int
+            Number of motors. Must be >= 2.
+        radius : float
+            Distance from center of rocket to center of motor (m).
+        """
+        if not isinstance(number, int):
+            raise TypeError(f"number must be an int, got {type(number).__name__}")
+        if number < 2:
+            raise ValueError("number must be >= 2 for a ClusterMotor")
+        if not isinstance(radius, (int, float)):
+            raise TypeError(
+                f"radius must be a real number, got {type(radius).__name__}"
+            )
+        if radius < 0:
+            raise ValueError("radius must be non-negative")
+
+        self.motor = motor
+        self.number = number
+        self.radius = float(radius)
+        dry_inertia_cluster = self._calculate_dry_inertia()
+
+        # Use a thrust source scaled by the number of motors so that
+        # all thrust-derived quantities computed by the base Motor class
+        # correspond to the full cluster rather than a single motor.
+        scaled_thrust_source = motor.thrust * number
+
+        super().__init__(
+            thrust_source=scaled_thrust_source,
+            nozzle_radius=motor.nozzle_radius,
+            burn_time=motor.burn_time,
+            dry_mass=motor.dry_mass * number,
+            dry_inertia=dry_inertia_cluster,
+            center_of_dry_mass_position=motor.center_of_dry_mass_position,
+            coordinate_system_orientation=motor.coordinate_system_orientation,
+            reference_pressure=motor.reference_pressure,
+            interpolation_method="linear",
+        )
+
+        # The cluster has ``number`` nozzles, so its total exit area (used for
+        # the pressure-thrust / vacuum-thrust correction, which must be
+        # consistent with the thrust that was scaled by ``number``) is
+        # ``number`` times a single nozzle's area. ``nozzle_radius`` is kept as
+        # the single-nozzle radius.
+        self.nozzle_area = np.pi * motor.nozzle_radius**2 * number
+
+        self._setup_grain_properties()
+        self._propellant_mass = self.motor.propellant_mass * self.number
+        self._propellant_initial_mass = self.number * self.motor.propellant_initial_mass
+        self._center_of_propellant_mass = self.motor.center_of_propellant_mass
+        self._evaluate_propellant_inertia()
+
+    def _evaluate_propellant_inertia(self):
+        """Calculates the dynamic inertia of the propellant using Steiner's theorem."""
+        self._propellant_I_11 = self.motor.propellant_I_11 * self.number
+        self._propellant_I_22 = self.motor.propellant_I_22 * self.number
+
+        angles = np.linspace(0, 2 * np.pi, self.number, endpoint=False)
+        for angle in angles:
+            x = self.radius * np.cos(angle)
+            y = self.radius * np.sin(angle)
+
+            self._propellant_I_11 += self.motor.propellant_mass * (y**2)
+            self._propellant_I_22 += self.motor.propellant_mass * (x**2)
+
+        Izz_term1 = self.motor.propellant_I_33 * self.number
+        Izz_term2 = self.motor.propellant_mass * (self.number * self.radius**2)
+        self._propellant_I_33 = Izz_term1 + Izz_term2
+
+        zero_func = Function(0)
+        self._propellant_I_12 = zero_func
+        self._propellant_I_13 = zero_func
+        self._propellant_I_23 = zero_func
+
+    @funcify_method("Time (s)", "Inertia I_22 (kg m²)")
+    def I_22(self):
+        """Assembled (dry + propellant) transverse inertia about the e_2 axis.
+
+        Overrides :meth:`Motor.I_22`, which returns ``I_11`` directly on the
+        assumption that the motor is axisymmetric. That assumption does not hold
+        for every ring cluster, so ``I_22`` is computed here from the
+        separately-evaluated ``_22`` components (see
+        :meth:`_evaluate_propellant_inertia` and :meth:`_calculate_dry_inertia`).
+
+        When ``I_22`` equals ``I_11``
+        -----------------------------
+        The relevant property is not continuous axisymmetry (which a discrete
+        cluster of ``number`` motors never has for finite ``number``) but
+        *transverse isotropy* of the inertia tensor: ``I_11 == I_22`` and
+        ``I_12 == 0``, i.e. every transverse axis is a principal axis with the
+        same moment. A rigid body has this whenever it possesses a discrete
+        rotational-symmetry axis of order ``n >= 3`` -- geometric axisymmetry is
+        sufficient but not necessary.
+
+        For a ring cluster the motors sit at angles ``theta_k = 2*pi*k/number``,
+        ``k = 0 .. number-1``, all at radius ``radius``. The transverse
+        anisotropy is driven by
+
+            I_22 - I_11  proportional to  sum_k (x_k**2 - y_k**2)
+                         = radius**2 * sum_k cos(2*theta_k)
+                         = radius**2 * Re( sum_k exp(i * 4*pi*k / number) ).
+
+        That geometric series vanishes unless ``exp(i*4*pi/number) == 1``, i.e.
+        unless ``number`` divides 2. Hence:
+
+        * ``number == 2`` -- the ``m = 2`` angular term does not cancel
+          (``sum cos(2*theta_k) == 2``); the cluster is transversely anisotropic
+          and ``I_22 != I_11``. This is the case this override exists for.
+        * ``number >= 3`` -- the term cancels exactly for *every* such value
+          (odd, even, prime alike); ``I_22 == I_11`` analytically, and this
+          method returns the same value as :meth:`I_11` up to floating-point
+          round-off.
+
+        Note that parity or primality of ``number`` is irrelevant: three or more
+        equally-spaced motors already annihilate the ``m = 2`` harmonic, so e.g.
+        ``number == 3`` and ``number == 5`` are both transversely isotropic. The
+        sole non-trivial anisotropic configuration (given the ``number >= 2``
+        constraint enforced in ``__init__``) is ``number == 2``.
+
+        The implementation nonetheless sums every motor's contribution
+        explicitly rather than special-casing ``number == 2``, so the result is
+        exact for all configurations.
+        """
+        prop_I_22 = parallel_axis_theorem_from_com(
+            self.propellant_I_22,
+            self.propellant_mass,
+            self.center_of_propellant_mass - self.center_of_mass,
+        )
+        dry_I_22 = parallel_axis_theorem_from_com(
+            self.dry_I_22,
+            self.dry_mass,
+            self.center_of_dry_mass_position - self.center_of_mass,
+        )
+        return prop_I_22 + dry_I_22
+
+    def _setup_grain_properties(self):
+        """Copies the grain properties from the base motor."""
+        self.throat_radius = self.motor.throat_radius
+        self.grain_number = self.motor.grain_number
+        self.grain_density = self.motor.grain_density
+        self.grain_outer_radius = self.motor.grain_outer_radius
+        self.grain_initial_inner_radius = self.motor.grain_initial_inner_radius
+        self.grain_initial_height = self.motor.grain_initial_height
+        self.grains_center_of_mass_position = self.motor.grains_center_of_mass_position
+
+    @property
+    def thrust(self):
+        return self._thrust
+
+    @thrust.setter
+    def thrust(self, value):
+        self._thrust = value
+
+    @property
+    def propellant_mass(self):
+        return self._propellant_mass
+
+    @propellant_mass.setter
+    def propellant_mass(self, value):
+        self._propellant_mass = value
+
+    @property
+    def propellant_initial_mass(self):
+        return self._propellant_initial_mass
+
+    @propellant_initial_mass.setter
+    def propellant_initial_mass(self, value):
+        self._propellant_initial_mass = value
+
+    @property
+    def center_of_propellant_mass(self):
+        return self._center_of_propellant_mass
+
+    @center_of_propellant_mass.setter
+    def center_of_propellant_mass(self, value):
+        self._center_of_propellant_mass = value
+
+    @property
+    def propellant_I_11(self):
+        return self._propellant_I_11
+
+    @propellant_I_11.setter
+    def propellant_I_11(self, value):
+        self._propellant_I_11 = value
+
+    @property
+    def propellant_I_22(self):
+        return self._propellant_I_22
+
+    @propellant_I_22.setter
+    def propellant_I_22(self, value):
+        self._propellant_I_22 = value
+
+    @property
+    def propellant_I_33(self):
+        return self._propellant_I_33
+
+    @propellant_I_33.setter
+    def propellant_I_33(self, value):
+        self._propellant_I_33 = value
+
+    @property
+    def propellant_I_12(self):
+        return self._propellant_I_12
+
+    @propellant_I_12.setter
+    def propellant_I_12(self, value):
+        self._propellant_I_12 = value
+
+    @property
+    def propellant_I_13(self):
+        return self._propellant_I_13
+
+    @propellant_I_13.setter
+    def propellant_I_13(self, value):
+        self._propellant_I_13 = value
+
+    @property
+    def propellant_I_23(self):
+        return self._propellant_I_23
+
+    @propellant_I_23.setter
+    def propellant_I_23(self, value):
+        self._propellant_I_23 = value
+
+    @property
+    def exhaust_velocity(self):
+        return self.motor.exhaust_velocity
+
+    def _calculate_dry_inertia(self):
+        Ixx_loc = self.motor.dry_I_11
+        Iyy_loc = self.motor.dry_I_22
+        Izz_loc = self.motor.dry_I_33
+        m_dry = self.motor.dry_mass
+
+        Izz_cluster = self.number * Izz_loc + self.number * m_dry * (self.radius**2)
+        Ixx_cluster = self.number * Ixx_loc
+        Iyy_cluster = self.number * Iyy_loc
+
+        angles = np.linspace(0, 2 * np.pi, self.number, endpoint=False)
+        for angle in angles:
+            x = self.radius * np.cos(angle)
+            y = self.radius * np.sin(angle)
+            Ixx_cluster += m_dry * (y**2)
+            Iyy_cluster += m_dry * (x**2)
+
+        return (Ixx_cluster, Iyy_cluster, Izz_cluster)
+
+    def info(self, *args, **kwargs):
+        print("Cluster Configuration:")
+        print(f" - Motors: {self.number} x {type(self.motor).__name__}")
+        print(f" - Radial Distance: {self.radius} m")
+        return self.motor.info(*args, **kwargs)
+
+    def to_dict(self, **kwargs):
+        data = super().to_dict(**kwargs)
+        data.update(
+            {
+                "motor": self.motor,
+                "number": self.number,
+                "radius": self.radius,
+            }
+        )
+        return data
+
+    @classmethod
+    def from_dict(cls, data):
+        return cls(
+            motor=data["motor"],
+            number=data["number"],
+            radius=data["radius"],
+        )
+
+    def draw_cluster_layout(self, rocket_radius=None, show=True):
+        """Draw the geometric layout of the clustered motors."""
+        fig, ax = plt.subplots(figsize=(6, 6))
+        ax.plot(0, 0, "k+", markersize=10, label="Central axis")
+        if rocket_radius:
+            rocket_tube = plt.Circle(
+                (0, 0),
+                rocket_radius,
+                color="black",
+                fill=False,
+                linestyle="--",
+                linewidth=2,
+                label="Rocket",
+            )
+            ax.add_patch(rocket_tube)
+            limit = rocket_radius * 1.2
+        else:
+            limit = self.radius * 2
+        self._draw_engines(ax)
+        ax.set_aspect("equal", "box")
+        ax.set_xlim(-limit, limit)
+        ax.set_ylim(-limit, limit)
+        ax.set_xlabel("Position X (m)")
+        ax.set_ylabel("Position Y (m)")
+        ax.set_title(f"Cluster Configuration : {self.number} engines")
+        ax.grid(True, linestyle=":", alpha=0.6)
+        ax.legend(loc="upper right")
+        if show:
+            plt.show()
+        return fig, ax
+
+    def _draw_engines(self, ax):
+        """Draws the individual engines of the cluster."""
+        motor_outer_radius = self.grain_outer_radius
+        angles = np.linspace(0, 2 * np.pi, self.number, endpoint=False)
+
+        for i, angle in enumerate(angles):
+            x = self.radius * np.cos(angle)
+            y = self.radius * np.sin(angle)
+            motor_circle = plt.Circle(
+                (x, y),
+                motor_outer_radius,
+                color="red",
+                alpha=0.5,
+                label="Engine" if i == 0 else "",
+            )
+            ax.add_patch(motor_circle)
+            ax.text(
+                x,
+                y,
+                str(i + 1),
+                color="white",
+                ha="center",
+                va="center",
+                fontweight="bold",
+            )
diff --git a/rocketpy/motors/tank.py b/rocketpy/motors/tank.py
index 6f3496b32..0d6b329a4 100644
--- a/rocketpy/motors/tank.py
+++ b/rocketpy/motors/tank.py
@@ -6,7 +6,7 @@
 from ..mathutils.function import Function, funcify_method
 from ..plots.tank_plots import _TankPlots
 from ..prints.tank_prints import _TankPrints
-from ..tools import deprecated, tuple_handler
+from ..tools import tuple_handler
 
 
 class Tank(ABC):
@@ -1025,17 +1025,6 @@ def _discretize_fluid_inputs(self):
             )
             self._gas_density.set_discrete_based_on_model(self.gas_mass_flow_rate_in)
 
-    @deprecated(
-        "Should not be a public member of the class.",
-        "1.12.0",
-        "_discretize_fluid_inputs",
-    )
-    def discretize_flow(self):
-        """Discretizes the mass flow rate inputs according to the flux time and
-        the discretize parameter.
-        """
-        self._discretize_fluid_inputs()
-
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
         data.update(
@@ -1288,17 +1277,6 @@ def _discretize_fluid_inputs(self):
             self._liquid_density.set_discrete_based_on_model(self.ullage)
             self._gas_density.set_discrete_based_on_model(self.ullage)
 
-    @deprecated(
-        "Should not be a public member of the class.",
-        "1.12.0",
-        "_discretize_fluid_inputs",
-    )
-    def discretize_ullage(self):
-        """Discretizes the ullage input according to the flux time
-        and the discretize parameter.
-        """
-        self._discretize_fluid_inputs()
-
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
         data.update({"ullage": self.ullage})
@@ -1542,17 +1520,6 @@ def gas_height(self):
             self.liquid_level
         )
 
-    @deprecated(
-        "Should not be a public member of the class.",
-        "1.12.0",
-        "_discretize_fluid_inputs",
-    )
-    def discretize_liquid_height(self):
-        """Discretizes the liquid height input according to the flux time
-        and the discretize parameter.
-        """
-        self._discretize_fluid_inputs()
-
     def _discretize_fluid_inputs(self):
         """Uniformly discretizes the parameter of inputs of fluid data ."""
         if self.discretize:
@@ -1835,17 +1802,6 @@ def gas_height(self):
             )
         return gas_height
 
-    @deprecated(
-        "Should not be a public member of the class.",
-        "1.12.0",
-        "_discretize_fluid_inputs",
-    )
-    def discretize_masses(self):
-        """Discretizes the fluid mass inputs according to the flux time
-        and the discretize parameter.
-        """
-        self._discretize_fluid_inputs()
-
     def _discretize_fluid_inputs(self):
         """Uniformly discretizes the parameter of inputs of fluid data ."""
         if self.discretize:
diff --git a/rocketpy/motors/tank_geometry.py b/rocketpy/motors/tank_geometry.py
index 485f57b09..e71f862ca 100644
--- a/rocketpy/motors/tank_geometry.py
+++ b/rocketpy/motors/tank_geometry.py
@@ -1,3 +1,5 @@
+import logging
+import warnings
 from functools import cached_property
 
 import numpy as np
@@ -7,6 +9,8 @@
 from ..plots.tank_geometry_plots import _TankGeometryPlots
 from ..prints.tank_geometry_prints import _TankGeometryPrints
 
+logger = logging.getLogger(__name__)
+
 try:
     from functools import cache
 except ImportError:
@@ -384,14 +388,21 @@ class inherits from the TankGeometry class. See the TankGeometry class
     for more information on its attributes and methods.
     """
 
-    def __init__(self, radius, height, spherical_caps=False, geometry_dict=None):
+    def __init__(
+        self,
+        radius_function=None,
+        height=None,
+        spherical_caps=False,
+        geometry_dict=None,
+        **kwargs,
+    ):
         """Initialize CylindricalTank class. The zero reference point of the
         cylinder is its center (i.e. half of its height). Therefore the its
         height coordinate span is (-height/2, height/2).
 
         Parameters
         ----------
-        radius : float
+        radius_function : int, float
             Radius of the cylindrical tank, in meters.
         height : float
             Height of the cylindrical tank, in meters.
@@ -401,17 +412,52 @@ def __init__(self, radius, height, spherical_caps=False, geometry_dict=None):
             will have flat caps at the top and bottom. Defaults to False.
         geometry_dict : Union[dict, None], optional
             Dictionary containing the geometry of the tank. See TankGeometry.
-        """
+
+        Notes
+        -----
+        The ``radius`` keyword argument is deprecated. Use ``radius_function``
+        instead.
+        """
+        if "radius" in kwargs:
+            if radius_function is not None:
+                raise TypeError(
+                    "Cannot specify both 'radius_function' and deprecated "
+                    "'radius' arguments. Use 'radius_function' instead."
+                )
+            warnings.warn(
+                "The 'radius' argument in CylindricalTank is deprecated in v1.13.0 "
+                "and will be removed in v2.0.0. Use 'radius_function' instead.",
+                DeprecationWarning,
+                stacklevel=2,
+            )
+            radius_function = kwargs.pop("radius")
+        if kwargs:
+            raise TypeError(
+                "CylindricalTank.__init__() got unexpected keyword argument(s): "
+                f"{', '.join(map(repr, kwargs))}"
+            )
+        if radius_function is None:
+            raise TypeError(
+                "CylindricalTank.__init__() missing required argument: "
+                "'radius_function'"
+            )
+        if height is None:
+            raise TypeError(
+                "CylindricalTank.__init__() missing required argument: 'height'"
+            )
         geometry_dict = geometry_dict or {}
         super().__init__(geometry_dict)
-        self.__input_radius = radius
+        self.radius_function = radius_function
         self.height = height
         self.has_caps = False
         if spherical_caps:
-            self.add_geometry((-height / 2 + radius, height / 2 - radius), radius)
+            self.add_geometry(
+                (-height / 2 + radius_function, height / 2 - radius_function),
+                radius_function,
+            )
             self.add_spherical_caps()
         else:
-            self.add_geometry((-height / 2, height / 2), radius)
+            self.add_geometry((-height / 2, height / 2), radius_function)
 
     def add_spherical_caps(self):
         """
@@ -420,15 +466,16 @@ def add_spherical_caps(self):
         part. The height is not modified, meaning that the total volume of
         the tank will decrease.
         """
-        print(
-            "Warning: Adding spherical caps to the tank will not modify the "
-            + f"total height of the tank {self.height} m. "
-            + "Its cylindrical portion height will be reduced to "
-            + f"{self.height - 2 * self.__input_radius} m."
+        logger.warning(
+            "Adding spherical caps to the tank will not modify the total height "
+            "of the tank (%.4f m). Its cylindrical portion height will be "
+            "reduced to %s m.",
+            self.height,
+            self.height - 2 * self.radius_function,
         )
 
         if not self.has_caps:
-            radius = self.__input_radius
+            radius = self.radius_function
             height = self.height
             bottom_cap_range = (-height / 2, -height / 2 + radius)
             upper_cap_range = (height / 2 - radius, height / 2)
@@ -447,7 +494,7 @@ def upper_cap_radius(h):
 
     def to_dict(self, **kwargs):
         data = {
-            "radius": self.__input_radius,
+            "radius_function": self.radius_function,
             "height": self.height,
             "spherical_caps": self.has_caps,
         }
@@ -459,7 +506,18 @@ def to_dict(self, **kwargs):
 
     @classmethod
     def from_dict(cls, data):
-        return cls(data["radius"], data["height"], data["spherical_caps"])
+        if "radius_function" in data:
+            radius_function = data["radius_function"]
+        else:
+            warnings.warn(
+                "The 'radius' key in CylindricalTank serialized data is "
+                "deprecated in v1.13.0 and will be removed in v2.0.0. "
+                "Use 'radius_function' instead.",
+                DeprecationWarning,
+                stacklevel=2,
+            )
+            radius_function = data["radius"]
+        return cls(radius_function, data["height"], data["spherical_caps"])
 
 
 class SphericalTank(TankGeometry):
@@ -468,25 +526,55 @@ class SphericalTank(TankGeometry):
     inherits from the TankGeometry class. See the TankGeometry class for
     more information on its attributes and methods."""
 
-    def __init__(self, radius, geometry_dict=None):
+    def __init__(self, radius_function=None, geometry_dict=None, **kwargs):
         """Initialize SphericalTank class. The zero reference point of the
         sphere is its center (i.e. half of its height). Therefore, its height
-        coordinate ranges between (-radius, radius).
+        coordinate ranges between (-radius_function, radius_function).
 
         Parameters
         ----------
-        radius : float
-            Radius of the spherical tank.
+        radius_function : int, float
+            Radius of the spherical tank, in meters.
         geometry_dict : Union[dict, None], optional
             Dictionary containing the geometry of the tank. See TankGeometry.
-        """
+
+        Notes
+        -----
+        The ``radius`` keyword argument is deprecated. Use ``radius_function``
+        instead.
+        """
+        if "radius" in kwargs:
+            if radius_function is not None:
+                raise TypeError(
+                    "Cannot specify both 'radius_function' and deprecated "
+                    "'radius' arguments. Use 'radius_function' instead."
+                )
+            warnings.warn(
+                "The 'radius' argument in SphericalTank is deprecated in v1.13.0 "
+                "and will be removed in v2.0.0. Use 'radius_function' instead.",
+                DeprecationWarning,
+                stacklevel=2,
+            )
+            radius_function = kwargs.pop("radius")
+        if kwargs:
+            raise TypeError(
+                "SphericalTank.__init__() got unexpected keyword argument(s): "
+                f"{', '.join(map(repr, kwargs))}"
+            )
+        if radius_function is None:
+            raise TypeError(
+                "SphericalTank.__init__() missing required argument: 'radius_function'"
+            )
         geometry_dict = geometry_dict or {}
         super().__init__(geometry_dict)
-        self.__input_radius = radius
-        self.add_geometry((-radius, radius), lambda h: (radius**2 - h**2) ** 0.5)
+        self.radius_function = radius_function
+        self.add_geometry(
+            (-radius_function, radius_function),
+            lambda h: (radius_function**2 - h**2) ** 0.5,
+        )
 
     def to_dict(self, **kwargs):
-        data = {"radius": self.__input_radius}
+        data = {"radius_function": self.radius_function}
 
         if kwargs.get("include_outputs", False):
             data.update(super().to_dict(**kwargs))
@@ -495,4 +583,15 @@ def to_dict(self, **kwargs):
 
     @classmethod
     def from_dict(cls, data):
-        return cls(data["radius"])
+        if "radius_function" in data:
+            radius_function = data["radius_function"]
+        else:
+            warnings.warn(
+                "The 'radius' key in SphericalTank serialized data is "
+                "deprecated in v1.13.0 and will be removed in v2.0.0. "
+                "Use 'radius_function' instead.",
+                DeprecationWarning,
+                stacklevel=2,
+            )
+            radius_function = data["radius"]
+        return cls(radius_function)
diff --git a/rocketpy/plots/aero_surface_plots.py b/rocketpy/plots/aero_surface_plots.py
index 397ad8f55..eb97ce19b 100644
--- a/rocketpy/plots/aero_surface_plots.py
+++ b/rocketpy/plots/aero_surface_plots.py
@@ -1,3 +1,5 @@
+# pylint: disable=too-many-statements
+
 from abc import ABC, abstractmethod
 
 import matplotlib.pyplot as plt
@@ -139,14 +141,97 @@ class _FinsPlots(_AeroSurfacePlots):
     """Abstract class that contains all fin plots. This class inherits from the
     _AeroSurfacePlots class."""
 
-    @abstractmethod
-    def draw(self, *, filename=None):
-        pass
+    def airfoil(self, *, filename=None):
+        """Plots the airfoil information when the fin has an airfoil shape. If
+        the fin does not have an airfoil shape, this method does nothing.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
+        Returns
+        -------
+        None
+        """
+
+        if self.aero_surface.airfoil:
+            print("Airfoil lift curve:")
+            self.aero_surface.airfoil_cl.plot_1d(force_data=True, filename=filename)
+
+    def roll(self, *, filename=None):
+        """Plots the roll parameters of the fin set.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
+        Returns
+        -------
+        None
+        """
+        print("Roll parameters:")
+        self.aero_surface.roll_parameters[0](filename=filename)
+        self.aero_surface.roll_parameters[1](filename=filename)
+
+    def lift(self, *, filename=None):
+        """Plots the lift coefficient of the aero surface as a function of Mach
+        and the angle of attack. A 3D plot is expected. See the rocketpy.Function
+        class for more information on how this plot is made. Also, this method
+        plots the lift coefficient considering a single fin and the lift
+        coefficient considering all fins.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
+        Returns
+        -------
+        None
+        """
+        print("Lift coefficient:")
+        self.aero_surface.cl(filename=filename)
+        self.aero_surface.clalpha_single_fin(filename=filename)
+        self.aero_surface.clalpha_multiple_fins(filename=filename)
+
+    def all(self, *, filename=None):
+        """Plots all available fin plots.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
+        Returns
+        -------
+        None
+        """
+        self.draw(filename=filename)
+        self.airfoil(filename=filename)
+        self.roll(filename=filename)
+        self.lift(filename=filename)
 
-    def airfoil(self):
+
+class _FinPlots(_AeroSurfacePlots):
+    """Abstract class that contains all fin plots. This class inherits from the
+    _AeroSurfacePlots class."""
+
+    def airfoil(self, *, filename=None):
         """Plots the airfoil information when the fin has an airfoil shape. If
         the fin does not have an airfoil shape, this method does nothing.
 
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
         Returns
         -------
         None
@@ -154,52 +239,68 @@ def airfoil(self):
 
         if self.aero_surface.airfoil:
             print("Airfoil lift curve:")
-            self.aero_surface.airfoil_cl.plot_1d(force_data=True)
+            self.aero_surface.airfoil_cl.plot_1d(force_data=True, filename=filename)
 
-    def roll(self):
+    def roll(self, *, filename=None):
         """Plots the roll parameters of the fin set.
 
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
         Returns
         -------
         None
         """
         print("Roll parameters:")
-        self.aero_surface.roll_parameters[0]()
-        self.aero_surface.roll_parameters[1]()
+        self.aero_surface.roll_parameters[0](filename=filename)
+        self.aero_surface.roll_parameters[1](filename=filename)
 
-    def lift(self):
+    def lift(self, *, filename=None):
         """Plots the lift coefficient of the aero surface as a function of Mach
         and the angle of attack. A 3D plot is expected. See the rocketpy.Function
         class for more information on how this plot is made. Also, this method
         plots the lift coefficient considering a single fin and the lift
         coefficient considering all fins.
 
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
         Returns
         -------
         None
         """
         print("Lift coefficient:")
-        self.aero_surface.cl()
-        self.aero_surface.clalpha_single_fin()
-        self.aero_surface.clalpha_multiple_fins()
+        self.aero_surface.cl(filename=filename)
+        self.aero_surface.clalpha_single_fin(filename=filename)
 
-    def all(self):
+    def all(self, *, filename=None):
         """Plots all available fin plots.
 
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved.
+
         Returns
         -------
         None
         """
-        self.draw()
-        self.airfoil()
-        self.roll()
-        self.lift()
+        self.draw(filename=filename)
+        self.airfoil(filename=filename)
+        self.roll(filename=filename)
+        self.lift(filename=filename)
 
 
 class _TrapezoidalFinsPlots(_FinsPlots):
     """Class that contains all trapezoidal fin plots."""
 
-    # pylint: disable=too-many-statements
     def draw(self, *, filename=None):
         """Draw the fin shape along with some important information, including
         the center line, the quarter line and the center of pressure position.
@@ -325,10 +426,129 @@ def draw(self, *, filename=None):
         show_or_save_plot(filename)
 
 
+class _TrapezoidalFinPlots(_FinPlots):
+    """Class that contains all trapezoidal fin plots."""
+
+    def draw(self, *, filename=None):
+        """Draw the fin shape along with some important information, including
+        the center line, the quarter line and the center of pressure position.
+
+        Returns
+        -------
+        None
+        """
+        # Color cycle [#348ABD, #A60628, #7A68A6, #467821, #D55E00, #CC79A7,
+        # #56B4E9, #009E73, #F0E442, #0072B2]
+        # Fin
+        leading_edge = plt.Line2D(
+            (0, self.aero_surface.sweep_length),
+            (0, self.aero_surface.span),
+            color="#A60628",
+        )
+        tip = plt.Line2D(
+            (
+                self.aero_surface.sweep_length,
+                self.aero_surface.sweep_length + self.aero_surface.tip_chord,
+            ),
+            (self.aero_surface.span, self.aero_surface.span),
+            color="#A60628",
+        )
+        back_edge = plt.Line2D(
+            (
+                self.aero_surface.sweep_length + self.aero_surface.tip_chord,
+                self.aero_surface.root_chord,
+            ),
+            (self.aero_surface.span, 0),
+            color="#A60628",
+        )
+        root = plt.Line2D((self.aero_surface.root_chord, 0), (0, 0), color="#A60628")
+
+        # Center and Quarter line
+        center_line = plt.Line2D(
+            (
+                self.aero_surface.root_chord / 2,
+                self.aero_surface.sweep_length + self.aero_surface.tip_chord / 2,
+            ),
+            (0, self.aero_surface.span),
+            color="#7A68A6",
+            alpha=0.35,
+            linestyle="--",
+            label="Center Line",
+        )
+        quarter_line = plt.Line2D(
+            (
+                self.aero_surface.root_chord / 4,
+                self.aero_surface.sweep_length + self.aero_surface.tip_chord / 4,
+            ),
+            (0, self.aero_surface.span),
+            color="#7A68A6",
+            alpha=1,
+            linestyle="--",
+            label="Quarter Line",
+        )
+
+        # Center of pressure
+        cp_point = [self.aero_surface.cpz, self.aero_surface.Yma]
+
+        # Mean Aerodynamic Chord
+        yma_start = (
+            self.aero_surface.sweep_length
+            * (self.aero_surface.root_chord + 2 * self.aero_surface.tip_chord)
+            / (3 * (self.aero_surface.root_chord + self.aero_surface.tip_chord))
+        )
+        yma_end = (
+            2 * self.aero_surface.root_chord**2
+            + self.aero_surface.root_chord * self.aero_surface.sweep_length
+            + 2 * self.aero_surface.root_chord * self.aero_surface.tip_chord
+            + 2 * self.aero_surface.sweep_length * self.aero_surface.tip_chord
+            + 2 * self.aero_surface.tip_chord**2
+        ) / (3 * (self.aero_surface.root_chord + self.aero_surface.tip_chord))
+        yma_line = plt.Line2D(
+            (yma_start, yma_end),
+            (self.aero_surface.Yma, self.aero_surface.Yma),
+            color="#467821",
+            linestyle="--",
+            label="Mean Aerodynamic Chord",
+        )
+
+        # Plotting
+        fig = plt.figure(figsize=(7, 4))
+        with plt.style.context("bmh"):
+            ax = fig.add_subplot(111)
+
+        # Fin
+        ax.add_line(leading_edge)
+        ax.add_line(tip)
+        ax.add_line(back_edge)
+        ax.add_line(root)
+
+        ax.add_line(center_line)
+        ax.add_line(quarter_line)
+        ax.add_line(yma_line)
+        ax.scatter(*cp_point, label="Center of Pressure", color="red", s=100, zorder=10)
+        ax.scatter(*cp_point, facecolors="none", edgecolors="red", s=500, zorder=10)
+
+        # Plot settings
+        xlim = (
+            self.aero_surface.root_chord
+            if self.aero_surface.sweep_length + self.aero_surface.tip_chord
+            < self.aero_surface.root_chord
+            else self.aero_surface.sweep_length + self.aero_surface.tip_chord
+        )
+        ax.set_xlim(0, xlim * 1.1)
+        ax.set_ylim(0, self.aero_surface.span * 1.1)
+        ax.set_xlabel("Root chord (m)")
+        ax.set_ylabel("Span (m)")
+        ax.set_title("Trapezoidal Fin Cross Section")
+        ax.legend(bbox_to_anchor=(1.05, 1.0), loc="upper left")
+
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+
 class _EllipticalFinsPlots(_FinsPlots):
     """Class that contains all elliptical fin plots."""
 
-    # pylint: disable=too-many-statements
     def draw(self, *, filename=None):
         """Draw the fin shape along with some important information.
         These being: the center line and the center of pressure position.
@@ -404,10 +624,153 @@ def draw(self, *, filename=None):
         show_or_save_plot(filename)
 
 
+class _EllipticalFinPlots(_FinPlots):
+    """Class that contains all elliptical fin plots."""
+
+    def draw(self, *, filename=None):
+        """Draw the fin shape along with some important information.
+        These being: the center line and the center of pressure position.
+
+        Returns
+        -------
+        None
+        """
+        # Ellipse
+        ellipse = Ellipse(
+            (self.aero_surface.root_chord / 2, 0),
+            self.aero_surface.root_chord,
+            self.aero_surface.span * 2,
+            fill=False,
+            edgecolor="#A60628",
+            linewidth=2,
+        )
+
+        # Mean Aerodynamic Chord # From Barrowman's theory
+        yma_length = 8 * self.aero_surface.root_chord / (3 * np.pi)
+        yma_start = (self.aero_surface.root_chord - yma_length) / 2
+        yma_end = (
+            self.aero_surface.root_chord
+            - (self.aero_surface.root_chord - yma_length) / 2
+        )
+        yma_line = plt.Line2D(
+            (yma_start, yma_end),
+            (self.aero_surface.Yma, self.aero_surface.Yma),
+            label="Mean Aerodynamic Chord",
+            color="#467821",
+        )
+
+        # Center Line
+        center_line = plt.Line2D(
+            (self.aero_surface.root_chord / 2, self.aero_surface.root_chord / 2),
+            (0, self.aero_surface.span),
+            color="#7A68A6",
+            alpha=0.35,
+            linestyle="--",
+            label="Center Line",
+        )
+
+        # Center of pressure
+        cp_point = [self.aero_surface.cpz, self.aero_surface.Yma]
+
+        # Plotting
+        fig = plt.figure(figsize=(7, 4))
+        with plt.style.context("bmh"):
+            ax = fig.add_subplot(111)
+        ax.add_patch(ellipse)
+        ax.add_line(yma_line)
+        ax.add_line(center_line)
+        ax.scatter(*cp_point, label="Center of Pressure", color="red", s=100, zorder=10)
+        ax.scatter(*cp_point, facecolors="none", edgecolors="red", s=500, zorder=10)
+
+        # Plot settings
+        ax.set_xlim(0, self.aero_surface.root_chord)
+        ax.set_ylim(0, self.aero_surface.span * 1.1)
+        ax.set_xlabel("Root chord (m)")
+        ax.set_ylabel("Span (m)")
+        ax.set_title("Elliptical Fin Cross Section")
+        ax.legend(bbox_to_anchor=(1.05, 1.0), loc="upper left")
+
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+
 class _FreeFormFinsPlots(_FinsPlots):
     """Class that contains all free form fin plots."""
 
-    # pylint: disable=too-many-statements
+    def draw(self, *, filename=None):
+        """Draw the fin shape along with some important information.
+        These being: the center line and the center of pressure position.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved. Supported file endings are:
+            eps, jpg, jpeg, pdf, pgf, png, ps, raw, rgba, svg, svgz, tif, tiff
+            and webp (these are the formats supported by matplotlib).
+
+        Returns
+        -------
+        None
+        """
+        # Color cycle [#348ABD, #A60628, #7A68A6, #467821, #D55E00, #CC79A7,
+        # #56B4E9, #009E73, #F0E442, #0072B2]
+
+        # Center of pressure
+        cp_point = [self.aero_surface.cpz, self.aero_surface.Yma]
+
+        # Mean Aerodynamic Chord
+        yma_line = plt.Line2D(
+            (
+                self.aero_surface.mac_lead,
+                self.aero_surface.mac_lead + self.aero_surface.mac_length,
+            ),
+            (self.aero_surface.Yma, self.aero_surface.Yma),
+            color="#467821",
+            linestyle="--",
+            label="Mean Aerodynamic Chord",
+        )
+
+        # Plotting
+        fig = plt.figure(figsize=(7, 4))
+        with plt.style.context("bmh"):
+            ax = fig.add_subplot(111)
+
+        # Fin
+        ax.scatter(
+            self.aero_surface.shape_vec[0],
+            self.aero_surface.shape_vec[1],
+            color="#A60628",
+        )
+        ax.plot(
+            self.aero_surface.shape_vec[0],
+            self.aero_surface.shape_vec[1],
+            color="#A60628",
+        )
+        # line from the last point to the first point
+        ax.plot(
+            [self.aero_surface.shape_vec[0][-1], self.aero_surface.shape_vec[0][0]],
+            [self.aero_surface.shape_vec[1][-1], self.aero_surface.shape_vec[1][0]],
+            color="#A60628",
+        )
+
+        ax.add_line(yma_line)
+        ax.scatter(*cp_point, label="Center of Pressure", color="red", s=100, zorder=10)
+        ax.scatter(*cp_point, facecolors="none", edgecolors="red", s=500, zorder=10)
+
+        # Plot settings
+        ax.set_xlabel("Root chord (m)")
+        ax.set_ylabel("Span (m)")
+        ax.set_title("Free Form Fin Cross Section")
+        ax.legend(bbox_to_anchor=(1.05, 1.0), loc="upper left")
+
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+
+class _FreeFormFinPlots(_FinPlots):
+    """Class that contains all free form fin plots."""
+
     def draw(self, *, filename=None):
         """Draw the fin shape along with some important information.
         These being: the center line and the center of pressure position.
diff --git a/rocketpy/plots/assets/default_rocket.stl b/rocketpy/plots/assets/default_rocket.stl
new file mode 100644
index 000000000..a8ee68d7c
--- /dev/null
+++ b/rocketpy/plots/assets/default_rocket.stl
@@ -0,0 +1,674 @@
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diff --git a/rocketpy/plots/compare/compare_flights.py b/rocketpy/plots/compare/compare_flights.py
index 4ff064858..0694d333c 100644
--- a/rocketpy/plots/compare/compare_flights.py
+++ b/rocketpy/plots/compare/compare_flights.py
@@ -1,11 +1,15 @@
 # TODO: remove this disable once the code is refactored
 # pylint: disable=nested-min-max
+import logging
+
 import matplotlib.pyplot as plt
 import numpy as np
 
 from ..plot_helpers import show_or_save_fig, show_or_save_plot
 from .compare import Compare
 
+logger = logging.getLogger(__name__)
+
 # TODO: needs to refactor this class to use the show_or_save_plot
 
 
@@ -94,7 +98,7 @@ def __process_savefig(self, filename, fig):
         """
         show_or_save_fig(fig, filename)
         if filename:
-            print("Plot saved to file: " + filename)
+            logger.info("Plot saved to file: %s", filename)
         else:
             plt.show()
 
@@ -1084,7 +1088,7 @@ def stability_margin(
         None
         """
 
-        print("This method is not implemented yet")
+        logger.warning("This method is not implemented yet.")
 
     def attitude_frequency(
         self,
@@ -1123,7 +1127,7 @@ def attitude_frequency(
         None
         """
 
-        print("This method is not implemented yet")
+        logger.warning("This method is not implemented yet.")
 
     @staticmethod
     def compare_trajectories_3d(  # pylint: disable=too-many-statements
diff --git a/rocketpy/plots/flight_plots.py b/rocketpy/plots/flight_plots.py
index 7eb41a8b2..e255831be 100644
--- a/rocketpy/plots/flight_plots.py
+++ b/rocketpy/plots/flight_plots.py
@@ -1,10 +1,17 @@
+import logging
+import os
+import time
 from functools import cached_property
+from importlib import resources
 
 import matplotlib.pyplot as plt
 import numpy as np
 
+from ..tools import import_optional_dependency
 from .plot_helpers import show_or_save_plot
 
+logger = logging.getLogger(__name__)
+
 
 class _FlightPlots:
     """Class that holds plot methods for Flight class.
@@ -133,6 +140,278 @@ def trajectory_3d(self, *, filename=None):  # pylint: disable=too-many-statement
         ax1.set_box_aspect(None, zoom=0.95)  # 95% for label adjustment
         show_or_save_plot(filename)
 
+    def _resolve_animation_model_path(self, file_name):
+        """Resolve model path, defaulting to the built-in STL when omitted."""
+        if file_name is not None:
+            return file_name
+
+        return str(
+            resources.files("rocketpy.plots").joinpath("assets/default_rocket.stl")
+        )
+
+    def _validate_animation_inputs(self, file_name, start, stop, time_step):
+        """Validate shared input parameters for 3D animation methods."""
+        if time_step <= 0:
+            raise ValueError(
+                f"Invalid time_step: {time_step}. It must be greater than 0."
+            )
+
+        if stop is None:
+            stop = self.flight.t_final
+
+        if (
+            start < 0
+            or stop < 0
+            or start > self.flight.t_final
+            or stop > self.flight.t_final
+            or start >= stop
+        ):
+            raise ValueError(
+                f"Invalid animation time range: start={start}, stop={stop}. "
+                f"Both must be within [0, {self.flight.t_final}] and start < stop."
+            )
+
+        if not os.path.isfile(file_name):
+            raise FileNotFoundError(
+                f"Could not find the 3D model file: '{file_name}'. "
+                "Provide a valid .stl file path."
+            )
+
+        return stop
+
+    @staticmethod
+    def _rotation_from_quaternion(q0, q1, q2, q3):
+        """Convert unit quaternion to axis-angle representation in degrees."""
+        norm = np.sqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3)
+        if norm == 0:
+            return 0.0, (1.0, 0.0, 0.0)
+
+        q0 = q0 / norm
+        q1 = q1 / norm
+        q2 = q2 / norm
+        q3 = q3 / norm
+
+        # q and -q represent the same orientation. Keep q0 non-negative to
+        # reduce discontinuities in axis-angle interpolation across frames.
+        if q0 < 0:
+            q0 = -q0
+            q1 = -q1
+            q2 = -q2
+            q3 = -q3
+
+        q0 = np.clip(q0, -1.0, 1.0)
+        angle = 2 * np.arccos(q0)
+        sin_half = np.sqrt(max(1 - q0 * q0, 0.0))
+
+        if sin_half < 1e-12:
+            return 0.0, (1.0, 0.0, 0.0)
+
+        axis = (q1 / sin_half, q2 / sin_half, q3 / sin_half)
+        return np.degrees(angle), axis
+
+    def _create_animation_box(self, start, scale=1.0):
+        """Create a world box with minimum visible dimensions."""
+        min_box_dim = 10.0
+        x_values = self.flight.x[:, 1]
+        y_values = self.flight.y[:, 1]
+        z_values = self.flight.z[:, 1] - self.flight.env.elevation
+
+        center_x = 0.5 * (np.max(x_values) + np.min(x_values))
+        center_y = 0.5 * (np.max(y_values) + np.min(y_values))
+        center_z = max(self.flight.z(start) - self.flight.env.elevation, 0.0)
+
+        length = max(np.ptp(x_values) * scale, min_box_dim)
+        width = max(np.ptp(y_values) * scale, min_box_dim)
+        height = max(np.ptp(z_values) * scale, min_box_dim)
+
+        # Keep z center inside visible space while preserving minimum box size.
+        center_z = max(center_z, 0.5 * min_box_dim)
+
+        vedo = import_optional_dependency("vedo")
+
+        return vedo.Box(
+            pos=[center_x, center_y, center_z],
+            length=length,
+            width=width,
+            height=height,
+        ).wireframe()
+
+    @staticmethod
+    def _require_interactive_vedo_backend(vedo):
+        """Ensure vedo can open an interactive VTK window for the animation.
+
+        The animations drive an interactive render loop, which needs a desktop
+        window. In Jupyter/headless environments vedo defaults to the ``"2d"``
+        backend, where every ``render()`` call fails with the cryptic
+        ``"No active Plotter found for the 2d backend"``. Fail early with a
+        clear, actionable message instead.
+        """
+        if getattr(vedo.settings, "default_backend", None) == "2d":
+            raise RuntimeError(
+                "Rocket animations require an interactive VTK window, which is "
+                "not available with vedo's '2d' backend (the default inside "
+                "Jupyter notebooks and headless environments). Run this from a "
+                "Python script, or switch vedo to a desktop backend before "
+                "calling it:\n"
+                "    import vedo\n"
+                "    vedo.settings.default_backend = 'vtk'"
+            )
+
+    def animate_trajectory(  # pylint: disable=too-many-statements
+        self, file_name=None, start=0, stop=None, time_step=0.1, **kwargs
+    ):
+        """Animate 6-DOF trajectory and attitude using vedo.
+
+        Parameters
+        ----------
+        file_name : str | None, optional
+            Path to a 3D model file representing the rocket, usually ``.stl``.
+            If None, RocketPy uses a built-in default STL model.
+            Default is None.
+        start : int, float, optional
+            Animation start time in seconds. Default is 0.
+        stop : int, float | None, optional
+            Animation end time in seconds. If None, uses ``flight.t_final``.
+            Default is None.
+        time_step : float, optional
+            Animation frame step in seconds. Must be greater than 0.
+            Default is 0.1.
+        **kwargs : dict, optional
+            Additional keyword arguments passed to ``vedo.Plotter.show``.
+        """
+
+        vedo = import_optional_dependency("vedo")
+        self._require_interactive_vedo_backend(vedo)
+
+        file_name = self._resolve_animation_model_path(file_name)
+        stop = self._validate_animation_inputs(file_name, start, stop, time_step)
+
+        try:
+            vedo.settings.allow_interaction = True
+        except AttributeError:
+            pass
+
+        world = self._create_animation_box(start, scale=1.2)
+        base_rocket = vedo.Mesh(file_name).c("green")
+        time_steps = np.arange(start, stop, time_step)
+        trajectory_points = []
+
+        plt = vedo.Plotter(axes=1, interactive=False)
+        plt.show(world, "Rocket Trajectory Animation", viewup="z", **kwargs)
+
+        for t in time_steps:
+            rocket = base_rocket.clone()
+            x_position = self.flight.x(t)
+            y_position = self.flight.y(t)
+            z_position = self.flight.z(t) - self.flight.env.elevation
+
+            angle_deg, axis = self._rotation_from_quaternion(
+                self.flight.e0(t),
+                self.flight.e1(t),
+                self.flight.e2(t),
+                self.flight.e3(t),
+            )
+
+            rocket.pos(x_position, y_position, z_position)
+            if angle_deg != 0.0:
+                # Rotate about the rocket's placed position. vedo's rotate()
+                # rotates about the world origin by default, which would map the
+                # model to R @ pos and displace it from its trajectory point.
+                rocket.rotate(
+                    angle_deg,
+                    axis=axis,
+                    point=(x_position, y_position, z_position),
+                )
+
+            trajectory_points.append([x_position, y_position, z_position])
+            actors = [world, rocket]
+            if len(trajectory_points) > 1:
+                actors.append(vedo.Line(trajectory_points, c="k", alpha=0.5))
+
+            plt.show(*actors, resetcam=False)
+
+            start_pause = time.time()
+            while time.time() - start_pause < time_step:
+                plt.render()
+                time.sleep(0.001)  # yield the CPU instead of busy-spinning
+
+            if getattr(plt, "escaped", False):
+                break
+
+        plt.interactive().close()
+
+    def animate_rotate(  # pylint: disable=too-many-statements
+        self, file_name=None, start=0, stop=None, time_step=0.1, **kwargs
+    ):
+        """Animate rocket attitude (rotation-only view) using vedo.
+
+        Parameters
+        ----------
+        file_name : str | None, optional
+            Path to a 3D model file representing the rocket, usually ``.stl``.
+            If None, RocketPy uses a built-in default STL model.
+            Default is None.
+        start : int, float, optional
+            Animation start time in seconds. Default is 0.
+        stop : int, float | None, optional
+            Animation end time in seconds. If None, uses ``flight.t_final``.
+            Default is None.
+        time_step : float, optional
+            Animation frame step in seconds. Must be greater than 0.
+            Default is 0.1.
+        **kwargs : dict, optional
+            Additional keyword arguments passed to ``vedo.Plotter.show``.
+        """
+
+        vedo = import_optional_dependency("vedo")
+        self._require_interactive_vedo_backend(vedo)
+
+        file_name = self._resolve_animation_model_path(file_name)
+        stop = self._validate_animation_inputs(file_name, start, stop, time_step)
+
+        try:
+            vedo.settings.allow_interaction = True
+        except AttributeError:
+            pass
+
+        world = self._create_animation_box(start, scale=0.3)
+        base_rocket = vedo.Mesh(file_name).c("green")
+        time_steps = np.arange(start, stop, time_step)
+
+        x_start = self.flight.x(start)
+        y_start = self.flight.y(start)
+        z_start = self.flight.z(start) - self.flight.env.elevation
+
+        plt = vedo.Plotter(axes=1, interactive=False)
+        plt.show(world, "Rocket Rotation Animation", viewup="z", **kwargs)
+
+        for t in time_steps:
+            rocket = base_rocket.clone()
+            angle_deg, axis = self._rotation_from_quaternion(
+                self.flight.e0(t),
+                self.flight.e1(t),
+                self.flight.e2(t),
+                self.flight.e3(t),
+            )
+
+            rocket.pos(x_start, y_start, z_start)
+            if angle_deg != 0.0:
+                # Rotate about the rocket's placed position (vedo rotates about
+                # the world origin by default, which would displace the model).
+                rocket.rotate(angle_deg, axis=axis, point=(x_start, y_start, z_start))
+
+            plt.show(world, rocket, resetcam=False)
+
+            start_pause = time.time()
+            while time.time() - start_pause < time_step:
+                plt.render()
+                time.sleep(0.001)  # yield the CPU instead of busy-spinning
+
+            if getattr(plt, "escaped", False):
+                break
+
+        plt.interactive().close()
+
     def linear_kinematics_data(self, *, filename=None):  # pylint: disable=too-many-statements
         """Prints out all Kinematics graphs available about the Flight
 
@@ -411,16 +690,20 @@ def rail_buttons_bending_moments(self, *, filename=None):
         None
         """
         if len(self.flight.rocket.rail_buttons) == 0:
-            print(
+            logger.warning(
                 "No rail buttons were defined. Skipping rail button bending moment plots."
             )
         elif self.flight.out_of_rail_time_index == 0:
-            print("No rail phase was found. Skipping rail button bending moment plots.")
+            logger.warning(
+                "No rail phase was found. Skipping rail button bending moment plots."
+            )
         else:
             # Check if button_height is defined
             rail_buttons_tuple = self.flight.rocket.rail_buttons[0]
             if rail_buttons_tuple.component.button_height is None:
-                print("Rail button height not defined. Skipping bending moment plots.")
+                logger.warning(
+                    "Rail button height not defined. Skipping bending moment plots."
+                )
             else:
                 plt.figure(figsize=(9, 3))
 
@@ -475,9 +758,9 @@ def rail_buttons_forces(self, *, filename=None):  # pylint: disable=too-many-sta
         None
         """
         if len(self.flight.rocket.rail_buttons) == 0:
-            print("No rail buttons were defined. Skipping rail button plots.")
+            logger.warning("No rail buttons were defined. Skipping rail button plots.")
         elif self.flight.out_of_rail_time_index == 0:
-            print("No rail phase was found. Skipping rail button plots.")
+            logger.warning("No rail phase was found. Skipping rail button plots.")
         else:
             plt.figure(figsize=(9, 6))
 
@@ -771,6 +1054,18 @@ def energy_data(self, *, filename=None):  # pylint: disable=too-many-statements
         plt.subplots_adjust(hspace=1)
         show_or_save_plot(filename)
 
+    @staticmethod
+    def __signed_angle_ylim(angle_function, t_start, t_end, margin=5):
+        """Return ``(ymin, ymax)`` limits for a signed angle plotted between
+        ``t_start`` and ``t_end``. The range is based only on the samples inside
+        that time window so the full (positive and negative) oscillation is
+        visible, unlike a fixed floor at zero which would clip it.
+        """
+        data = angle_function[:, :]
+        mask = (data[:, 0] >= t_start) & (data[:, 0] <= t_end)
+        values = data[mask, 1] if np.any(mask) else data[:, 1]
+        return values.min() - margin, values.max() + margin
+
     def fluid_mechanics_data(self, *, filename=None):  # pylint: disable=too-many-statements
         """Prints out a summary of the Fluid Mechanics graphs available about
         the Flight
@@ -848,8 +1143,15 @@ def fluid_mechanics_data(self, *, filename=None):  # pylint: disable=too-many-st
         ax5.set_xlabel("Time (s)")
         ax5.set_ylabel("Partial Angle of Attack (°)")
         ax5.set_xlim(self.flight.out_of_rail_time, self.first_event_time)
+        # Partial angle of attack is a signed angle oscillating around zero, so
+        # scale to the data in the plotted window instead of flooring at 0
+        # (which would clip the negative half of the oscillation).
         ax5.set_ylim(
-            0, self.flight.partial_angle_of_attack(self.flight.out_of_rail_time) + 15
+            *self.__signed_angle_ylim(
+                self.flight.partial_angle_of_attack,
+                self.flight.out_of_rail_time,
+                self.first_event_time,
+            )
         )
         ax5.grid()
 
@@ -861,8 +1163,13 @@ def fluid_mechanics_data(self, *, filename=None):  # pylint: disable=too-many-st
         ax6.set_xlabel("Time (s)")
         ax6.set_ylabel("Angle of Sideslip (°)")
         ax6.set_xlim(self.flight.out_of_rail_time, self.first_event_time)
+        # Sideslip is also signed; keep the full oscillation visible.
         ax6.set_ylim(
-            0, self.flight.angle_of_sideslip(self.flight.out_of_rail_time) + 15
+            *self.__signed_angle_ylim(
+                self.flight.angle_of_sideslip,
+                self.flight.out_of_rail_time,
+                self.first_event_time,
+            )
         )
         ax6.grid()
 
@@ -1002,14 +1309,113 @@ def pressure_signals(self):
         None
         """
 
-        if len(self.flight.parachute_events) > 0:
-            for parachute in self.flight.rocket.parachutes:
-                print("\nParachute: ", parachute.name)
-                parachute.noise_signal_function()
-                parachute.noisy_pressure_signal_function()
-                parachute.clean_pressure_signal_function()
+        if len(self.flight.parachute_events) == 0:
+            logger.warning("Rocket has no parachutes. No parachute plots available.")
+            return
+
+        for parachute in self.flight.rocket.parachutes:
+            clean = parachute.clean_pressure_signal_function
+            noisy = parachute.noisy_pressure_signal_function
+            # Nothing was recorded (e.g. parachute never triggered)
+            if not isinstance(clean.source, np.ndarray) or clean.source.ndim != 2:
+                continue
+            time_signal = clean.source[:, 0]
+
+            plt.figure(figsize=(9, 4))
+            plt.plot(
+                time_signal, clean(time_signal), label="Without noise", linewidth=1.5
+            )
+            plt.plot(
+                time_signal,
+                noisy(time_signal),
+                label="With noise",
+                alpha=0.7,
+                linewidth=0.8,
+            )
+            plt.title(f"Parachute trigger pressure signal: {parachute.name}")
+            plt.xlabel("Time (s)")
+            plt.ylabel("Pressure (Pa)")
+            plt.legend()
+            plt.grid(True)
+            show_or_save_plot()
+
+    def parachutes_info(self, parachute_name="all"):
+        """Plots parachute dynamic information.
+        This function plots the dynamic relevant information to each parachute.
+        Different parachute models have different dynamic variables. It is
+        assumed that the 'parachutes_info' members have the dynamic variables
+        together with their respective time
+
+        Parameters
+        ----------
+        parachute_name : str | optional
+            The parachute name to display information. Default is 'all', in
+            which case information about all parachutes are plotted.
+
+        Returns
+        -------
+        None
+        """
+        # Parachute dynamic information (e.g. drag) is saved during
+        # post-processing, which is evaluated lazily. Accessing a post-processed
+        # variable forces it to run, so this plot works even when called before
+        # any other post-processed variable has been accessed.
+        _ = self.flight.ax
+
+        if not getattr(self.flight, "parachutes_info", None):
+            print("\nFlight has no parachute dynamic information available.")
+            return
+
+        if parachute_name == "all":
+            items = list(self.flight.parachutes_info.items())
+        elif parachute_name in self.flight.parachutes_info:
+            items = [(parachute_name, self.flight.parachutes_info[parachute_name])]
         else:
-            print("\nRocket has no parachutes. No parachute plots available")
+            print(
+                f"\nNo dynamic information available for parachute "
+                f"'{parachute_name}'. It may not have been deployed during the "
+                f"flight. Available parachutes: "
+                f"{list(self.flight.parachutes_info.keys())}."
+            )
+            return
+
+        # Gather every dynamic variable across the selected parachutes so each
+        # one is drawn on a single figure with all parachutes overlaid.
+        variables = []
+        for _, parachute_variables in items:
+            for variable in parachute_variables:
+                if variable != "t" and variable not in variables:
+                    variables.append(variable)
+
+        for variable in variables:
+            self.__plot_parachute_variable(variable, items)
+
+    # Axis label (and unit) for each known parachute dynamic variable.
+    __parachute_variable_labels = {"drag": ("Drag Force", "N")}
+
+    def __plot_parachute_variable(self, variable, items):
+        """Plot a single parachute dynamic variable (e.g. drag) for every
+        parachute in ``items`` overlaid on one figure, one colour each."""
+        label, unit = self.__parachute_variable_labels.get(
+            variable, (variable.replace("_", " ").title(), "")
+        )
+        ylabel = f"{label} ({unit})" if unit else label
+
+        plt.figure(figsize=(9, 4))
+        for name, parachute_variables in items:
+            if variable not in parachute_variables:
+                continue
+            plt.plot(
+                parachute_variables["t"],
+                parachute_variables[variable],
+                label=name,
+            )
+        plt.title(f"Parachute {label} vs Time")
+        plt.xlabel("Time (s)")
+        plt.ylabel(ylabel)
+        plt.legend()
+        plt.grid(True)
+        show_or_save_plot()
 
     def all(self):  # pylint: disable=too-many-statements
         """Prints out all plots available about the Flight.
@@ -1028,7 +1434,7 @@ def all(self):  # pylint: disable=too-many-statements
         print("\n\nAngular Position Plots\n")
         self.flight_path_angle_data()
 
-        print("\n\nPath, Attitude and Lateral Attitude Angle plots\n")
+        print("\n\nPath, Attitude and Lateral Attitude Angle Plots\n")
         self.attitude_data()
 
         print("\n\nTrajectory Angular Velocity and Acceleration Plots\n")
@@ -1055,3 +1461,4 @@ def all(self):  # pylint: disable=too-many-statements
         print("\n\nRocket and Parachute Pressure Plots\n")
         self.pressure_rocket_altitude()
         self.pressure_signals()
+        self.parachutes_info()
diff --git a/rocketpy/plots/monte_carlo_plots.py b/rocketpy/plots/monte_carlo_plots.py
index e9ce4ef3a..aeb0f2746 100644
--- a/rocketpy/plots/monte_carlo_plots.py
+++ b/rocketpy/plots/monte_carlo_plots.py
@@ -1,3 +1,4 @@
+import logging
 import urllib
 from pathlib import Path
 
@@ -14,6 +15,8 @@
 )
 from .plot_helpers import show_or_save_plot
 
+logger = logging.getLogger(__name__)
+
 
 class _MonteCarloPlots:
     """Class to plot the Monte Carlo analysis results."""
@@ -265,14 +268,14 @@ def ellipses(
             apogee_x = np.array(self.monte_carlo.results["apogee_x"])
             apogee_y = np.array(self.monte_carlo.results["apogee_y"])
         except KeyError:
-            print("No apogee data found. Skipping apogee ellipses.")
+            logger.warning("No apogee data found. Skipping apogee ellipses.")
             apogee_x = np.array([])
             apogee_y = np.array([])
         try:
             impact_x = np.array(self.monte_carlo.results["x_impact"])
             impact_y = np.array(self.monte_carlo.results["y_impact"])
         except KeyError:
-            print("No impact data found. Skipping impact ellipses.")
+            logger.warning("No impact data found. Skipping impact ellipses.")
             impact_x = np.array([])
             impact_y = np.array([])
 
@@ -557,7 +560,7 @@ def ellipses_comparison(
             other_apogee_x = np.array(other_monte_carlo.results["apogee_x"])
             other_apogee_y = np.array(other_monte_carlo.results["apogee_y"])
         except KeyError:
-            print("No apogee data found. Skipping apogee ellipses.")
+            logger.warning("No apogee data found. Skipping apogee ellipses.")
             original_apogee_x = np.array([])
             original_apogee_y = np.array([])
             other_apogee_x = np.array([])
@@ -568,7 +571,7 @@ def ellipses_comparison(
             other_impact_x = np.array(other_monte_carlo.results["x_impact"])
             other_impact_y = np.array(other_monte_carlo.results["y_impact"])
         except KeyError:
-            print("No impact data found. Skipping impact ellipses.")
+            logger.warning("No impact data found. Skipping impact ellipses.")
             original_impact_x = np.array([])
             original_impact_y = np.array([])
             other_impact_x = np.array([])
diff --git a/rocketpy/plots/rocket_plots.py b/rocketpy/plots/rocket_plots.py
index e208c775f..8e2b35558 100644
--- a/rocketpy/plots/rocket_plots.py
+++ b/rocketpy/plots/rocket_plots.py
@@ -1,8 +1,9 @@
 import matplotlib.pyplot as plt
 import numpy as np
 
-from rocketpy.motors import EmptyMotor, HybridMotor, LiquidMotor, SolidMotor
-from rocketpy.rocket.aero_surface import Fins, NoseCone, Tail
+from rocketpy.mathutils.vector_matrix import Vector
+from rocketpy.motors import HybridMotor, LiquidMotor, SolidMotor
+from rocketpy.rocket.aero_surface import Fin, Fins, NoseCone, Tail
 from rocketpy.rocket.aero_surface.generic_surface import GenericSurface
 
 from .plot_helpers import show_or_save_plot
@@ -183,7 +184,7 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
             and webp (these are the formats supported by matplotlib).
         """
 
-        self.__validate_aerodynamic_surfaces()
+        self.__validate_aerodynamic_surfaces(plane)
 
         if vis_args is None:
             vis_args = {
@@ -203,9 +204,9 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
 
         csys = self.rocket._csys
         reverse = csys == 1
-        self.rocket.aerodynamic_surfaces.sort_by_position(reverse=reverse)
+        surfaces = self.rocket.aerodynamic_surfaces.sort_by_position(reverse=reverse)
 
-        drawn_surfaces = self._draw_aerodynamic_surfaces(ax, vis_args, plane)
+        drawn_surfaces = self._draw_aerodynamic_surfaces(ax, vis_args, plane, surfaces)
         last_radius, last_x = self._draw_tubes(ax, drawn_surfaces, vis_args)
         self._draw_motor(last_radius, last_x, ax, vis_args)
         self._draw_rail_buttons(ax, vis_args)
@@ -221,13 +222,15 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
         plt.tight_layout()
         show_or_save_plot(filename)
 
-    def __validate_aerodynamic_surfaces(self):
+    def __validate_aerodynamic_surfaces(self, plane):
         if not self.rocket.aerodynamic_surfaces:
             raise ValueError(
                 "The rocket must have at least one aerodynamic surface to be drawn."
             )
+        if plane not in ("xz", "yz"):
+            raise ValueError("The plane must be 'xz' or 'yz'. The default is 'xz'.")
 
-    def _draw_aerodynamic_surfaces(self, ax, vis_args, plane):
+    def _draw_aerodynamic_surfaces(self, ax, vis_args, plane, surfaces):
         """Draws the aerodynamic surfaces and saves the position of the points
         of interest for the tubes."""
         # List of drawn surfaces with the position of points of interest
@@ -240,13 +243,17 @@ def _draw_aerodynamic_surfaces(self, ax, vis_args, plane):
         # diameter changes. The final point of the last surface is the final
         # point of the last tube
 
-        for surface, position in self.rocket.aerodynamic_surfaces:
+        for surface, position in surfaces:
             if isinstance(surface, NoseCone):
                 self._draw_nose_cone(ax, surface, position.z, drawn_surfaces, vis_args)
             elif isinstance(surface, Tail):
                 self._draw_tail(ax, surface, position.z, drawn_surfaces, vis_args)
             elif isinstance(surface, Fins):
-                self._draw_fins(ax, surface, position.z, drawn_surfaces, vis_args)
+                self._draw_fins(
+                    ax, surface, position.z, drawn_surfaces, vis_args, plane
+                )
+            elif isinstance(surface, Fin):
+                self._draw_fin(ax, surface, position, drawn_surfaces, vis_args, plane)
             elif isinstance(surface, GenericSurface):
                 self._draw_generic_surface(
                     ax, surface, position, drawn_surfaces, vis_args, plane
@@ -309,13 +316,15 @@ def _draw_tail(self, ax, surface, position, drawn_surfaces, vis_args):
         # Add the tail to the list of drawn surfaces
         drawn_surfaces.append((surface, position, surface.bottom_radius, x_tail[-1]))
 
-    def _draw_fins(self, ax, surface, position, drawn_surfaces, vis_args):
+    def _draw_fins(self, ax, surface, position, drawn_surfaces, vis_args, plane):
         """Draws the fins and saves the position of the points of interest
         for the tubes."""
         num_fins = surface.n
         x_fin = -self.rocket._csys * surface.shape_vec[0] + position
         y_fin = surface.shape_vec[1] + surface.rocket_radius
-        rotation_angles = [2 * np.pi * i / num_fins for i in range(num_fins)]
+        rotation_angles = np.array([2 * np.pi * i / num_fins for i in range(num_fins)])
+        if plane == "xz":
+            rotation_angles -= np.pi / 2
 
         for angle in rotation_angles:
             # Create a rotation matrix for the current angle around the x-axis
@@ -327,13 +336,6 @@ def _draw_fins(self, ax, surface, position, drawn_surfaces, vis_args):
             # Extract x and y coordinates of the rotated points
             x_rotated, y_rotated = rotated_points_2d
 
-            # Project points above the XY plane back into the XY plane (set z-coordinate to 0)
-            x_rotated = np.where(
-                rotated_points_2d[1] > 0, rotated_points_2d[0], x_rotated
-            )
-            y_rotated = np.where(
-                rotated_points_2d[1] > 0, rotated_points_2d[1], y_rotated
-            )
             ax.plot(
                 x_rotated,
                 y_rotated,
@@ -343,6 +345,56 @@ def _draw_fins(self, ax, surface, position, drawn_surfaces, vis_args):
 
         drawn_surfaces.append((surface, position, surface.rocket_radius, x_rotated[-1]))
 
+    def _draw_fin(self, ax, surface, position, drawn_surfaces, vis_args, plane):
+        """Draws individual fins."""
+
+        # Get shape vec
+        xs = surface.shape_vec[0]
+        ys = surface.shape_vec[1]
+        zs = np.zeros_like(xs)
+
+        # Define shape in fin coordinate system
+        x_fin = -zs
+        y_fin = ys
+        z_fin = xs
+        points = np.column_stack((x_fin, y_fin, z_fin))
+
+        # Move drawing coordinates to center of fin for cant angle rotation
+        xd = np.array([0, 0, max(xs) / 2])
+        points -= xd
+
+        # Rotate to body coordinate system
+        for i, p in enumerate(points):
+            points[i] = surface._rotation_fin_to_body @ Vector(p)
+
+        rotated_xd = surface._rotation_fin_to_body @ Vector(xd)
+        points += np.array(rotated_xd)
+
+        # Back to the drawing system
+        x_fin_rotated = points[:, 0]
+        y_fin_rotated = points[:, 1]
+        z_fin_rotated = points[:, 2]
+
+        if plane == "xz":
+            x_rotated = self.rocket._csys * z_fin_rotated + position.z
+            y_rotated = x_fin_rotated + position.x
+        elif plane == "yz":
+            x_rotated = self.rocket._csys * z_fin_rotated + position.z
+            y_rotated = y_fin_rotated + position.y
+        else:  # pragma: no cover
+            raise ValueError("Plane must be 'xz' or 'yz'.")
+
+        ax.plot(
+            x_rotated,
+            y_rotated,
+            color=vis_args["fins"],
+            linewidth=vis_args["line_width"],
+        )
+
+        drawn_surfaces.append(
+            (surface, position.z, surface.rocket_radius, x_rotated[-1])
+        )
+
     def _draw_generic_surface(
         self,
         ax,
@@ -420,57 +472,82 @@ def _draw_tubes(self, ax, drawn_surfaces, vis_args):
     def _draw_motor(self, last_radius, last_x, ax, vis_args):
         """Draws the motor from motor patches"""
         total_csys = self.rocket._csys * self.rocket.motor._csys
+        is_cluster = hasattr(self.rocket.motor, "number")
+        base_motor = self.rocket.motor.motor if is_cluster else self.rocket.motor
+
+        if is_cluster:
+            angles = np.linspace(0, 2 * np.pi, self.rocket.motor.number, endpoint=False)
+            y_offsets = self.rocket.motor.radius * np.cos(angles)
+        else:
+            y_offsets = [0]
         nozzle_position = (
-            self.rocket.motor_position + self.rocket.motor.nozzle_position * total_csys
+            self.rocket.motor_position + base_motor.nozzle_position * total_csys
         )
-
         # Get motor patches translated to the correct position
         motor_patches = self._generate_motor_patches(total_csys, ax)
-
         # Draw patches
-        if not isinstance(self.rocket.motor, EmptyMotor):
-            # Add nozzle last so it is in front of the other patches
-            nozzle = self.rocket.motor.plots._generate_nozzle(
-                translate=(nozzle_position, 0), csys=self.rocket._csys
-            )
-            motor_patches += [nozzle]
+        if type(self.rocket.motor).__name__ != "EmptyMotor":
+            for y_off in y_offsets:
+                nozzle = base_motor.plots._generate_nozzle(
+                    translate=(nozzle_position, y_off), csys=self.rocket._csys
+                )
+                if y_off != y_offsets[0]:
+                    nozzle.set_label("_nolegend_")
+                motor_patches.append(nozzle)
 
-            outline = self.rocket.motor.plots._generate_motor_region(
+            outline = base_motor.plots._generate_motor_region(
                 list_of_patches=motor_patches
             )
-            # add outline first so it is behind the other patches
-            ax.add_patch(outline)
+            if not is_cluster:
+                ax.add_patch(outline)
+
             for patch in motor_patches:
+                if is_cluster:
+                    patch.set_alpha(0.6)
                 ax.add_patch(patch)
-
         self._draw_nozzle_tube(last_radius, last_x, nozzle_position, ax, vis_args)
 
-    def _generate_motor_patches(self, total_csys, ax):  # pylint: disable=unused-argument
+    def _generate_motor_patches(self, total_csys, ax):
         """Generates motor patches for drawing"""
         motor_patches = []
 
-        if isinstance(self.rocket.motor, SolidMotor):
+        is_cluster = hasattr(self.rocket.motor, "number")
+        base_motor = self.rocket.motor.motor if is_cluster else self.rocket.motor
+
+        if isinstance(base_motor, SolidMotor):
+            y_offsets = (
+                self.rocket.motor.radius
+                * np.cos(
+                    np.linspace(0, 2 * np.pi, self.rocket.motor.number, endpoint=False)
+                )
+                if is_cluster
+                else [0]
+            )
             grains_cm_position = (
                 self.rocket.motor_position
-                + self.rocket.motor.grains_center_of_mass_position * total_csys
-            )
-            ax.scatter(
-                grains_cm_position,
-                0,
-                color="brown",
-                label="Grains Center of Mass",
-                s=8,
-                zorder=10,
+                + base_motor.grains_center_of_mass_position * total_csys
             )
+            for y_off in y_offsets:
+                ax.scatter(
+                    grains_cm_position,
+                    y_off,
+                    color="brown",
+                    label="Grains Center of Mass" if y_off == y_offsets[0] else "",
+                    s=8,
+                    zorder=10,
+                )
 
-            chamber = self.rocket.motor.plots._generate_combustion_chamber(
-                translate=(grains_cm_position, 0), label=None
-            )
-            grains = self.rocket.motor.plots._generate_grains(
-                translate=(grains_cm_position, 0)
-            )
+                chamber = base_motor.plots._generate_combustion_chamber(
+                    translate=(grains_cm_position, y_off), label=None
+                )
+                grains = base_motor.plots._generate_grains(
+                    translate=(grains_cm_position, y_off)
+                )
+                if y_off != y_offsets[0]:
+                    for grain in grains:
+                        grain.set_label("_nolegend_")
 
-            motor_patches += [chamber, *grains]
+                motor_patches += [chamber, *grains]
 
         elif isinstance(self.rocket.motor, HybridMotor):
             grains_cm_position = (
@@ -654,7 +731,7 @@ def all(self):
 
         # Rocket draw
         if len(self.rocket.aerodynamic_surfaces) > 0:
-            print("\nRocket Draw")
+            print("\nRocket Drawing")
             print("-" * 40)
             self.draw()
 
diff --git a/rocketpy/prints/aero_surface_prints.py b/rocketpy/prints/aero_surface_prints.py
index 4eb42b08d..cc36f1b01 100644
--- a/rocketpy/prints/aero_surface_prints.py
+++ b/rocketpy/prints/aero_surface_prints.py
@@ -1,6 +1,7 @@
 from abc import ABC, abstractmethod
 
 
+# TODO: the rocketpy/prints/aero_surface_prints.py file could be separated into different, smaller files.
 class _AeroSurfacePrints(ABC):
     def __init__(self, aero_surface):
         self.aero_surface = aero_surface
@@ -77,10 +78,8 @@ def geometry(self):
         print("-------------------------------------")
         print(f"Number of fins: {self.aero_surface.n}")
         print(f"Reference rocket radius: {self.aero_surface.rocket_radius:.3f} m")
-        try:
+        if hasattr(self.aero_surface, "tip_chord"):
             print(f"Tip chord: {self.aero_surface.tip_chord:.3f} m")
-        except AttributeError:
-            pass  # it isn't a trapezoidal fin, just don't worry about tip chord
         print(f"Root chord: {self.aero_surface.root_chord:.3f} m")
         print(f"Span: {self.aero_surface.span:.3f} m")
         print(
@@ -156,9 +155,102 @@ def lift(self):
             "Lift Coefficient derivative (single fin) at Mach 0 and AoA 0: "
             f"{self.aero_surface.clalpha_single_fin(0):.3f}"
         )
+
+    def all(self):
+        """Prints all information of the fin set.
+
+        Returns
+        -------
+        None
+        """
+        self.identity()
+        self.geometry()
+        self.airfoil()
+        self.roll()
+        self.lift()
+
+
+class _FinPrints(_AeroSurfacePrints):
+    def geometry(self):
+        print("Geometric information of the fin set:")
+        print("-------------------------------------")
+        print(f"Reference rocket radius: {self.aero_surface.rocket_radius:.3f} m")
+        if hasattr(self.aero_surface, "tip_chord"):
+            print(f"Tip chord: {self.aero_surface.tip_chord:.3f} m")
+        print(f"Root chord: {self.aero_surface.root_chord:.3f} m")
+        print(f"Span: {self.aero_surface.span:.3f} m")
+        print(
+            f"Cant angle: {self.aero_surface.cant_angle:.3f} ° or "
+            f"{self.aero_surface.cant_angle_rad:.3f} rad"
+        )
+        print(f"Longitudinal section area: {self.aero_surface.Af:.3f} m²")
+        print(f"Aspect ratio: {self.aero_surface.AR:.3f} ")
+        print(f"Gamma_c: {self.aero_surface.gamma_c:.3f} m")
+        print(f"Mean aerodynamic chord: {self.aero_surface.Yma:.3f} m\n")
+
+    def airfoil(self):
+        """Prints out airfoil related information of the fin set.
+
+        Returns
+        -------
+        None
+        """
+        if self.aero_surface.airfoil:
+            print("Airfoil information:")
+            print("--------------------")
+            print(
+                "Number of points defining the lift curve: "
+                f"{len(self.aero_surface.airfoil_cl.x_array)}"
+            )
+            print(
+                "Lift coefficient derivative at Mach 0 and AoA 0: "
+                f"{self.aero_surface.clalpha(0):.5f} 1/rad\n"
+            )
+
+    def roll(self):
+        """Prints out information about roll parameters
+        of the fin set.
+
+        Returns
+        -------
+        None
+        """
+        print("Roll information of the fin set:")
+        print("--------------------------------")
+        print(
+            f"Geometric constant: {self.aero_surface.roll_geometrical_constant:.3f} m"
+        )
+        print(
+            "Damping interference factor: "
+            f"{self.aero_surface.roll_damping_interference_factor:.3f} rad"
+        )
+        print(
+            "Forcing interference factor: "
+            f"{self.aero_surface.roll_forcing_interference_factor:.3f} rad\n"
+        )
+
+    def lift(self):
+        """Prints out information about lift parameters
+        of the fin set.
+
+        Returns
+        -------
+        None
+        """
+        print("Lift information of the fin set:")
+        print("--------------------------------")
         print(
-            "Lift Coefficient derivative (fin set) at Mach 0 and AoA 0: "
-            f"{self.aero_surface.clalpha_multiple_fins(0):.3f}"
+            "Lift interference factor: "
+            f"{self.aero_surface.lift_interference_factor:.3f} m"
+        )
+        print(
+            "Center of Pressure position in local coordinates: "
+            f"({self.aero_surface.cpx:.3f}, {self.aero_surface.cpy:.3f}, "
+            f"{self.aero_surface.cpz:.3f})"
+        )
+        print(
+            "Lift Coefficient derivative (single fin) at Mach 0 and AoA 0: "
+            f"{self.aero_surface.clalpha_single_fin(0):.3f}"
         )
 
     def all(self):
@@ -179,14 +271,26 @@ class _TrapezoidalFinsPrints(_FinsPrints):
     """Class that contains all trapezoidal fins prints."""
 
 
+class _TrapezoidalFinPrints(_FinPrints):
+    """Class that contains all trapezoidal fin prints."""
+
+
 class _EllipticalFinsPrints(_FinsPrints):
     """Class that contains all elliptical fins prints."""
 
 
+class _EllipticalFinPrints(_FinPrints):
+    """Class that contains all elliptical fin prints."""
+
+
 class _FreeFormFinsPrints(_FinsPrints):
     """Class that contains all free form fins prints."""
 
 
+class _FreeFormFinPrints(_FinPrints):
+    """Class that contains all free form fins prints."""
+
+
 class _TailPrints(_AeroSurfacePrints):
     """Class that contains all tail prints."""
 
diff --git a/rocketpy/prints/controller_prints.py b/rocketpy/prints/controller_prints.py
index cb19ec00c..e2690c36a 100644
--- a/rocketpy/prints/controller_prints.py
+++ b/rocketpy/prints/controller_prints.py
@@ -41,7 +41,10 @@ def controller_function(self):
             print(
                 "Controller function: " + self.controller.controller_function.__name__
             )
-        print(f"Controller refresh rate: {self.controller.sampling_rate:.3f} Hz")
+        if self.controller.is_continuous:
+            print("Controller refresh rate: continuous (every solver step)")
+        else:
+            print(f"Controller refresh rate: {self.controller.sampling_rate:.3f} Hz")
 
     def interactive_objects(self):
         """Prints interactive objects."""
diff --git a/rocketpy/rocket/__init__.py b/rocketpy/rocket/__init__.py
index 463cbe3b3..6c45a6d1c 100644
--- a/rocketpy/rocket/__init__.py
+++ b/rocketpy/rocket/__init__.py
@@ -2,17 +2,21 @@
 from rocketpy.rocket.aero_surface import (
     AeroSurface,
     AirBrakes,
+    EllipticalFin,
     EllipticalFins,
+    Fin,
     Fins,
+    FreeFormFin,
     FreeFormFins,
     GenericSurface,
     LinearGenericSurface,
     NoseCone,
     RailButtons,
     Tail,
+    TrapezoidalFin,
     TrapezoidalFins,
 )
 from rocketpy.rocket.components import Components
-from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.parachutes import HemisphericalParachute, Parachute
 from rocketpy.rocket.point_mass_rocket import PointMassRocket
 from rocketpy.rocket.rocket import Rocket
diff --git a/rocketpy/rocket/aero_surface/__init__.py b/rocketpy/rocket/aero_surface/__init__.py
index ad784f8d0..7634d3500 100644
--- a/rocketpy/rocket/aero_surface/__init__.py
+++ b/rocketpy/rocket/aero_surface/__init__.py
@@ -1,9 +1,13 @@
 from rocketpy.rocket.aero_surface.aero_surface import AeroSurface
 from rocketpy.rocket.aero_surface.air_brakes import AirBrakes
 from rocketpy.rocket.aero_surface.fins import (
+    EllipticalFin,
     EllipticalFins,
+    Fin,
     Fins,
+    FreeFormFin,
     FreeFormFins,
+    TrapezoidalFin,
     TrapezoidalFins,
 )
 from rocketpy.rocket.aero_surface.generic_surface import GenericSurface
diff --git a/rocketpy/rocket/aero_surface/aero_surface.py b/rocketpy/rocket/aero_surface/aero_surface.py
index 15ca14f1d..6727476c6 100644
--- a/rocketpy/rocket/aero_surface/aero_surface.py
+++ b/rocketpy/rocket/aero_surface/aero_surface.py
@@ -2,6 +2,8 @@
 
 import numpy as np
 
+from rocketpy.mathutils.vector_matrix import Matrix
+
 
 class AeroSurface(ABC):
     """Abstract class used to define aerodynamic surfaces."""
@@ -15,6 +17,14 @@ def __init__(self, name, reference_area, reference_length):
         self.cpy = 0
         self.cpz = 0
 
+        self._rotation_surface_to_body = Matrix(
+            [
+                [-1, 0, 0],
+                [0, 1, 0],
+                [0, 0, -1],
+            ]
+        )
+
     @staticmethod
     def _beta(mach):
         """Defines a parameter that is often used in aerodynamic
@@ -130,7 +140,7 @@ def compute_forces_and_moments(
         R1, R2, R3, M1, M2, M3 = 0, 0, 0, 0, 0, 0
         cpz = cp[2]
         stream_vx, stream_vy, stream_vz = stream_velocity
-        if stream_vx**2 + stream_vy**2 != 0:  # TODO: maybe try/except
+        if stream_vx**2 + stream_vy**2 != 0:
             # Normalize component stream velocity in body frame
             stream_vzn = stream_vz / stream_speed
             if -1 * stream_vzn < 1:
diff --git a/rocketpy/rocket/aero_surface/fins/__init__.py b/rocketpy/rocket/aero_surface/fins/__init__.py
index 941aa5465..dd678c625 100644
--- a/rocketpy/rocket/aero_surface/fins/__init__.py
+++ b/rocketpy/rocket/aero_surface/fins/__init__.py
@@ -1,4 +1,8 @@
+from rocketpy.rocket.aero_surface.fins.elliptical_fin import EllipticalFin
 from rocketpy.rocket.aero_surface.fins.elliptical_fins import EllipticalFins
+from rocketpy.rocket.aero_surface.fins.fin import Fin
 from rocketpy.rocket.aero_surface.fins.fins import Fins
+from rocketpy.rocket.aero_surface.fins.free_form_fin import FreeFormFin
 from rocketpy.rocket.aero_surface.fins.free_form_fins import FreeFormFins
+from rocketpy.rocket.aero_surface.fins.trapezoidal_fin import TrapezoidalFin
 from rocketpy.rocket.aero_surface.fins.trapezoidal_fins import TrapezoidalFins
diff --git a/rocketpy/rocket/aero_surface/fins/_base_fin.py b/rocketpy/rocket/aero_surface/fins/_base_fin.py
new file mode 100644
index 000000000..f6b09f797
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/_base_fin.py
@@ -0,0 +1,344 @@
+import math
+from abc import abstractmethod
+
+import numpy as np
+
+from rocketpy.mathutils.function import Function
+
+from ..aero_surface import AeroSurface
+
+
+class _BaseFin(AeroSurface):
+    """
+    Base class for fins, shared by both Fin and Fins classes.
+    Inherits from AeroSurface.
+
+    Handles shared initialization logic and common properties.
+    """
+
+    def __init__(
+        self, name, rocket_radius, root_chord, span, airfoil=None, cant_angle=0
+    ):
+        """
+        Initialize the base fin class.
+
+        Parameters
+        ----------
+        name : str
+            Name of the fin or fin set.
+        rocket_radius : float
+            Rocket radius in meters.
+        root_chord : float
+            Root chord of the fin in meters.
+        span : float
+            Span of the fin in meters.
+        airfoil : tuple, optional
+            Tuple containing airfoil data and unit ('degrees' or 'radians').
+        cant_angle : float, optional
+            Cant angle in degrees.
+        """
+        self.name = name
+        self._rocket_radius = rocket_radius
+        self._root_chord = root_chord
+        self._span = span
+        self._airfoil = airfoil
+        self._cant_angle = cant_angle
+        self._cant_angle_rad = math.radians(cant_angle)
+        self.geometry = None
+
+        self.reference_area = np.pi * rocket_radius**2
+
+        super().__init__(name, self.reference_area, self.rocket_diameter)
+
+    def _update_reference_quantities(self):
+        """Update quantities that depend on rocket radius."""
+        self.reference_area = np.pi * self._rocket_radius**2
+        self.reference_length = self.rocket_diameter
+
+    def _update_geometry_chain(self):
+        """Update geometry-dependent quantities in dependency order."""
+        self.evaluate_geometrical_parameters()
+        self.evaluate_center_of_pressure()
+        self.evaluate_lift_coefficient()
+        self.evaluate_roll_parameters()
+
+    @property
+    def rocket_radius(self):
+        """Rocket radius in meters.
+
+        Returns
+        -------
+        float
+            Rocket radius in meters.
+        """
+        return self._rocket_radius
+
+    @rocket_radius.setter
+    def rocket_radius(self, value):
+        """Set rocket radius and update dependent properties.
+
+        Parameters
+        ----------
+        value : float
+            Rocket radius in meters.
+        """
+        self._rocket_radius = value
+        self._update_reference_quantities()
+        self._update_geometry_chain()
+
+    @property
+    def rocket_diameter(self):
+        """Reference rocket diameter in meters."""
+        return 2 * self._rocket_radius
+
+    @rocket_diameter.setter
+    def rocket_diameter(self, value):
+        """Set reference rocket diameter in meters."""
+        self.rocket_radius = value / 2
+
+    @property
+    def diameter(self):
+        """Backward-compatible alias for :attr:`rocket_diameter`."""
+        return self.rocket_diameter
+
+    @diameter.setter
+    def diameter(self, value):
+        """Backward-compatible alias setter for :attr:`rocket_diameter`."""
+        self.rocket_diameter = value
+
+    @property
+    def d(self):
+        """Backward-compatible alias for :attr:`rocket_diameter`."""
+        return self.rocket_diameter
+
+    @d.setter
+    def d(self, value):
+        """Backward-compatible alias setter for :attr:`rocket_diameter`."""
+        self.rocket_diameter = value
+
+    @property
+    def ref_area(self):
+        """Backward-compatible alias for :attr:`reference_area`."""
+        return self.reference_area
+
+    @ref_area.setter
+    def ref_area(self, value):
+        """Backward-compatible alias setter for :attr:`reference_area`."""
+        self.reference_area = value
+
+    @property
+    def root_chord(self):
+        """Root chord length in meters.
+
+        Returns
+        -------
+        float
+            Root chord length in meters.
+        """
+        return self._root_chord
+
+    @root_chord.setter
+    def root_chord(self, value):
+        """Set root chord and update dependent properties.
+
+        Parameters
+        ----------
+        value : float
+            Root chord length in meters.
+        """
+        self._root_chord = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
+
+    @property
+    def span(self):
+        """Fin span in meters.
+
+        Returns
+        -------
+        float
+            Fin span in meters.
+        """
+        return self._span
+
+    @span.setter
+    def span(self, value):
+        """Set fin span and update dependent properties.
+
+        Parameters
+        ----------
+        value : float
+            Fin span in meters.
+        """
+        self._span = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
+
+    @property
+    def cant_angle(self):
+        """Cant angle in degrees.
+
+        Returns
+        -------
+        float
+            Cant angle in degrees.
+        """
+        return self._cant_angle
+
+    @cant_angle.setter
+    def cant_angle(self, value):
+        """Set cant angle and update radian representation.
+
+        Parameters
+        ----------
+        value : float
+            Cant angle in degrees.
+        """
+        self._cant_angle = value
+        self.cant_angle_rad = math.radians(value)
+
+    @property
+    def cant_angle_rad(self):
+        """Cant angle in radians.
+
+        Returns
+        -------
+        float
+            Cant angle in radians.
+        """
+        return self._cant_angle_rad
+
+    @cant_angle_rad.setter
+    def cant_angle_rad(self, value):
+        """Set cant angle in radians and update dependent properties.
+
+        Parameters
+        ----------
+        value : float
+            Cant angle in radians.
+        """
+        self._cant_angle_rad = value
+        self._update_geometry_chain()
+
+    @property
+    def airfoil(self):
+        """Airfoil data for the fin.
+
+        Returns
+        -------
+        tuple or None
+            Tuple containing airfoil data and unit ('degrees' or 'radians'),
+            or None if using planar fin.
+        """
+        return self._airfoil
+
+    @airfoil.setter
+    def airfoil(self, value):
+        """Set airfoil data and update dependent properties.
+
+        Parameters
+        ----------
+        value : tuple or None
+            Tuple containing airfoil data and unit ('degrees' or 'radians'),
+            or None for planar fin.
+        """
+        self._airfoil = value
+        self._update_geometry_chain()
+
+    def info(self):
+        """Print fin geometry and lift information."""
+        self.prints.geometry()
+        self.prints.lift()
+
+    def all_info(self):
+        """Print all available fin information and show all fin plots."""
+        self.prints.all()
+        self.plots.all()
+
+    def evaluate_single_fin_lift_coefficient(self):
+        """Evaluate the lift coefficient derivative for a single fin.
+
+        Computes the lift coefficient derivative (clalpha) considering the
+        fin's geometry, airfoil characteristics (if provided), and Mach number
+        effects using Prandtl-Glauert compressibility correction and
+        Diederich's planform correlation.
+
+        Sets the `clalpha_single_fin` attribute as a Function of Mach number.
+        """
+        if not self.airfoil:
+            # Defines clalpha2D as 2*pi for planar fins
+            clalpha2D_incompressible = 2 * np.pi
+        else:
+            # Defines clalpha2D as the derivative of the lift coefficient curve
+            # for the specific airfoil
+            self.airfoil_cl = Function(
+                self.airfoil[0],
+                title="Airfoil lift coefficient",
+                interpolation="linear",
+            )
+
+            # Differentiating at alpha = 0 to get cl_alpha
+            clalpha2D_incompressible = self.airfoil_cl.differentiate(x=1e-3, dx=1e-3)
+
+            # Convert to radians if needed
+            if self.airfoil[1] == "degrees":
+                clalpha2D_incompressible *= 180 / np.pi
+
+        # Correcting for compressible flow (apply Prandtl-Glauert correction)
+        clalpha2D = Function(lambda mach: clalpha2D_incompressible / self._beta(mach))
+
+        # Diederich's Planform Correlation Parameter
+        planform_correlation_parameter = (
+            2 * np.pi * self.AR / (clalpha2D * np.cos(self.gamma_c))
+        )
+
+        # Lift coefficient derivative for a single fin
+        def lift_source(mach):
+            return (
+                clalpha2D(mach)
+                * planform_correlation_parameter(mach)
+                * (self.Af / self.reference_area)
+                * np.cos(self.gamma_c)
+            ) / (
+                2
+                + planform_correlation_parameter(mach)
+                * np.sqrt(1 + (2 / planform_correlation_parameter(mach)) ** 2)
+            )
+
+        self.clalpha_single_fin = Function(
+            lift_source,
+            "Mach",
+            "Lift coefficient derivative for a single fin",
+        )
+
+    @abstractmethod
+    def evaluate_lift_coefficient(self):
+        """Evaluate the lift coefficient for the fin."""
+
+    @abstractmethod
+    def evaluate_roll_parameters(self):
+        """Evaluate roll-related parameters for the fin."""
+
+    @abstractmethod
+    def evaluate_center_of_pressure(self):
+        """Evaluate the center of pressure for the fin."""
+
+    def evaluate_geometrical_parameters(self):
+        """Evaluate geometric parameters of the fin.
+
+        This method delegates to the configured geometry strategy.
+        """
+        geometry_data = self.geometry.evaluate_geometrical_parameters()
+        for key, value in geometry_data.items():
+            setattr(self, key, value)
+
+    def evaluate_shape(self):
+        """Evaluate the shape representation of the fin.
+
+        This method delegates to the configured geometry strategy.
+        """
+        self.shape_vec = self.geometry.evaluate_shape()
+
+    @abstractmethod
+    def draw(self):
+        """Draw or render the fin."""
diff --git a/rocketpy/rocket/aero_surface/fins/_geometry.py b/rocketpy/rocket/aero_surface/fins/_geometry.py
new file mode 100644
index 000000000..71b213909
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/_geometry.py
@@ -0,0 +1,564 @@
+"""Geometry strategy classes for fin aerodynamic surfaces."""
+
+import warnings
+from abc import ABC, abstractmethod
+
+import numpy as np
+
+
+class _FinGeometry(ABC):
+    """Base geometry strategy for fin shapes."""
+
+    def __init__(self, owner):
+        self.owner = owner
+
+    @abstractmethod
+    def evaluate_geometrical_parameters(self):
+        """Evaluate and return geometry-dependent aerodynamic parameters."""
+
+    @abstractmethod
+    def evaluate_shape(self):
+        """Evaluate and return the shape vector used by plotting and outputs."""
+
+    def get_data(self, include_outputs=False):
+        """Return geometry-specific serialization data."""
+        _ = include_outputs
+        return {}
+
+
+class _TrapezoidalGeometry(_FinGeometry):
+    """Geometry strategy for trapezoidal fins."""
+
+    def __init__(
+        self,
+        owner,
+        tip_chord,
+        sweep_length=None,
+        sweep_angle=None,
+    ):
+        super().__init__(owner)
+        if sweep_length is not None and sweep_angle is not None:
+            raise ValueError("Cannot use sweep_length and sweep_angle together")
+
+        if sweep_angle is not None:
+            sweep_length = np.tan(np.radians(sweep_angle)) * owner.span
+        elif sweep_length is None:
+            sweep_length = owner.root_chord - tip_chord
+
+        self._tip_chord = tip_chord
+        self._sweep_length = sweep_length
+        self._sweep_angle = sweep_angle
+
+    @property
+    def tip_chord(self):
+        return self._tip_chord
+
+    @tip_chord.setter
+    def tip_chord(self, value):
+        self._tip_chord = value
+
+    @property
+    def sweep_length(self):
+        return self._sweep_length
+
+    @sweep_length.setter
+    def sweep_length(self, value):
+        self._sweep_length = value
+
+    @property
+    def sweep_angle(self):
+        return self._sweep_angle
+
+    @sweep_angle.setter
+    def sweep_angle(self, value):
+        self._sweep_angle = value
+        self._sweep_length = np.tan(np.radians(value)) * self.owner.span
+
+    def evaluate_geometrical_parameters(self):
+        """Calculate trapezoidal fin geometric parameters."""
+        # pylint: disable=invalid-name
+        owner = self.owner
+        Yr = owner.root_chord + self.tip_chord
+        Af = Yr * owner.span / 2
+        AR = 2 * owner.span**2 / Af
+        gamma_c = np.arctan(
+            (self.sweep_length + 0.5 * self.tip_chord - 0.5 * owner.root_chord)
+            / owner.span
+        )
+        Yma = (owner.span / 3) * (owner.root_chord + 2 * self.tip_chord) / Yr
+
+        tau = (owner.span + owner.rocket_radius) / owner.rocket_radius
+        lift_interference_factor = 1 + 1 / tau
+        lambda_ = self.tip_chord / owner.root_chord
+
+        roll_geometrical_constant = (
+            (owner.root_chord + 3 * self.tip_chord) * owner.span**3
+            + 4
+            * (owner.root_chord + 2 * self.tip_chord)
+            * owner.rocket_radius
+            * owner.span**2
+            + 6
+            * (owner.root_chord + self.tip_chord)
+            * owner.span
+            * owner.rocket_radius**2
+        ) / 12
+        roll_damping_interference_factor = 1 + (
+            ((tau - lambda_) / tau) - ((1 - lambda_) / (tau - 1)) * np.log(tau)
+        ) / (
+            ((tau + 1) * (tau - lambda_)) / 2
+            - ((1 - lambda_) * (tau**3 - 1)) / (3 * (tau - 1))
+        )
+        roll_forcing_interference_factor = (1 / np.pi**2) * (
+            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
+            + (np.pi * (tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
+            + ((tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
+            - (4 * (tau + 1))
+            / (tau * (tau - 1))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
+        )
+
+        self.Yr = Yr
+        self.Af = Af
+        self.AR = AR
+        self.gamma_c = gamma_c
+        self.Yma = Yma
+        self.roll_geometrical_constant = roll_geometrical_constant
+        self.tau = tau
+        self.lift_interference_factor = lift_interference_factor
+        self.λ = lambda_  # pylint: disable=non-ascii-name
+        self.roll_damping_interference_factor = roll_damping_interference_factor
+        self.roll_forcing_interference_factor = roll_forcing_interference_factor
+
+        return {
+            "Yr": Yr,
+            "Af": Af,
+            "AR": AR,
+            "gamma_c": gamma_c,
+            "Yma": Yma,
+            "roll_geometrical_constant": roll_geometrical_constant,
+            "tau": tau,
+            "lift_interference_factor": lift_interference_factor,
+            "λ": lambda_,  # pylint: disable=non-ascii-name
+            "roll_damping_interference_factor": roll_damping_interference_factor,
+            "roll_forcing_interference_factor": roll_forcing_interference_factor,
+        }
+
+    def evaluate_shape(self):
+        owner = self.owner
+        if self.sweep_length:
+            points = [
+                (0, 0),
+                (self.sweep_length, owner.span),
+                (self.sweep_length + self.tip_chord, owner.span),
+                (owner.root_chord, 0),
+            ]
+        else:
+            points = [
+                (0, 0),
+                (owner.root_chord - self.tip_chord, owner.span),
+                (owner.root_chord, owner.span),
+                (owner.root_chord, 0),
+            ]
+
+        x_array, y_array = zip(*points)
+        shape_vec = [np.array(x_array), np.array(y_array)]
+        self.shape_vec = shape_vec
+        return shape_vec
+
+    def get_data(self, include_outputs=False):
+        data = {
+            "tip_chord": self.tip_chord,
+            "sweep_length": self.sweep_length,
+            "sweep_angle": self.sweep_angle,
+        }
+        if include_outputs:
+            data.update(
+                {
+                    "shape_vec": getattr(self, "shape_vec", None),
+                    "Af": getattr(self, "Af", None),
+                    "AR": getattr(self, "AR", None),
+                    "gamma_c": getattr(self, "gamma_c", None),
+                    "Yma": getattr(self, "Yma", None),
+                    "roll_geometrical_constant": getattr(
+                        self, "roll_geometrical_constant", None
+                    ),
+                    "tau": getattr(self, "tau", None),
+                    "lift_interference_factor": getattr(
+                        self, "lift_interference_factor", None
+                    ),
+                    "roll_damping_interference_factor": getattr(
+                        self, "roll_damping_interference_factor", None
+                    ),
+                    "roll_forcing_interference_factor": getattr(
+                        self, "roll_forcing_interference_factor", None
+                    ),
+                }
+            )
+        return data
+
+
+class _EllipticalGeometry(_FinGeometry):
+    """Geometry strategy for elliptical fins."""
+
+    def evaluate_geometrical_parameters(self):  # pylint: disable=too-many-statements
+        """Calculate elliptical fin geometric parameters."""
+        owner = self.owner
+
+        # pylint: disable=invalid-name
+        Af = (np.pi * owner.root_chord / 2 * owner.span) / 2
+        gamma_c = 0
+        AR = 2 * owner.span**2 / Af
+        Yma = owner.span / (3 * np.pi) * np.sqrt(9 * np.pi**2 - 64)
+        roll_geometrical_constant = (
+            owner.root_chord
+            * owner.span
+            * (
+                3 * np.pi * owner.span**2
+                + 32 * owner.rocket_radius * owner.span
+                + 12 * np.pi * owner.rocket_radius**2
+            )
+            / 48
+        )
+
+        tau = (owner.span + owner.rocket_radius) / owner.rocket_radius
+        lift_interference_factor = 1 + 1 / tau
+        if owner.span > owner.rocket_radius:
+            roll_damping_interference_factor = 1 + (
+                owner.rocket_radius**2
+                * (
+                    2
+                    * owner.rocket_radius**2
+                    * np.sqrt(owner.span**2 - owner.rocket_radius**2)
+                    * np.log(
+                        (
+                            2
+                            * owner.span
+                            * np.sqrt(owner.span**2 - owner.rocket_radius**2)
+                            + 2 * owner.span**2
+                        )
+                        / owner.rocket_radius
+                    )
+                    - 2
+                    * owner.rocket_radius**2
+                    * np.sqrt(owner.span**2 - owner.rocket_radius**2)
+                    * np.log(2 * owner.span)
+                    + 2 * owner.span**3
+                    - np.pi * owner.rocket_radius * owner.span**2
+                    - 2 * owner.rocket_radius**2 * owner.span
+                    + np.pi * owner.rocket_radius**3
+                )
+            ) / (
+                2
+                * owner.span**2
+                * (owner.span / 3 + np.pi * owner.rocket_radius / 4)
+                * (owner.span**2 - owner.rocket_radius**2)
+            )
+        elif owner.span < owner.rocket_radius:
+            roll_damping_interference_factor = 1 - (
+                owner.rocket_radius**2
+                * (
+                    2 * owner.span**3
+                    - np.pi * owner.span**2 * owner.rocket_radius
+                    - 2 * owner.span * owner.rocket_radius**2
+                    + np.pi * owner.rocket_radius**3
+                    + 2
+                    * owner.rocket_radius**2
+                    * np.sqrt(-(owner.span**2) + owner.rocket_radius**2)
+                    * np.arctan(
+                        owner.span / np.sqrt(-(owner.span**2) + owner.rocket_radius**2)
+                    )
+                    - np.pi
+                    * owner.rocket_radius**2
+                    * np.sqrt(-(owner.span**2) + owner.rocket_radius**2)
+                )
+            ) / (
+                2
+                * owner.span
+                * (-(owner.span**2) + owner.rocket_radius**2)
+                * (owner.span**2 / 3 + np.pi * owner.span * owner.rocket_radius / 4)
+            )
+        else:
+            roll_damping_interference_factor = (28 - 3 * np.pi) / (4 + 3 * np.pi)
+
+        roll_forcing_interference_factor = (1 / np.pi**2) * (
+            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
+            + (np.pi * (tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
+            + ((tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
+            - (4 * (tau + 1))
+            / (tau * (tau - 1))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
+        )
+
+        self.Af = Af
+        self.AR = AR
+        self.gamma_c = gamma_c
+        self.Yma = Yma
+        self.roll_geometrical_constant = roll_geometrical_constant
+        self.tau = tau
+        self.lift_interference_factor = lift_interference_factor
+        self.roll_damping_interference_factor = roll_damping_interference_factor
+        self.roll_forcing_interference_factor = roll_forcing_interference_factor
+
+        return {
+            "Af": Af,
+            "AR": AR,
+            "gamma_c": gamma_c,
+            "Yma": Yma,
+            "roll_geometrical_constant": roll_geometrical_constant,
+            "tau": tau,
+            "lift_interference_factor": lift_interference_factor,
+            "roll_damping_interference_factor": roll_damping_interference_factor,
+            "roll_forcing_interference_factor": roll_forcing_interference_factor,
+        }
+
+    def evaluate_shape(self):
+        owner = self.owner
+        angles = np.arange(0, 180, 5)
+        x_array = owner.root_chord / 2 + owner.root_chord / 2 * np.cos(
+            np.radians(angles)
+        )
+        y_array = owner.span * np.sin(np.radians(angles))
+        shape_vec = [x_array, y_array]
+        self.shape_vec = shape_vec
+        return shape_vec
+
+    def get_data(self, include_outputs=False):
+        if not include_outputs:
+            return {}
+        return {
+            "Af": getattr(self, "Af", None),
+            "AR": getattr(self, "AR", None),
+            "gamma_c": getattr(self, "gamma_c", None),
+            "Yma": getattr(self, "Yma", None),
+            "roll_geometrical_constant": getattr(
+                self, "roll_geometrical_constant", None
+            ),
+            "tau": getattr(self, "tau", None),
+            "lift_interference_factor": getattr(self, "lift_interference_factor", None),
+            "roll_damping_interference_factor": getattr(
+                self, "roll_damping_interference_factor", None
+            ),
+            "roll_forcing_interference_factor": getattr(
+                self, "roll_forcing_interference_factor", None
+            ),
+        }
+
+
+class _FreeFormGeometry(_FinGeometry):
+    """Geometry strategy for free-form fins."""
+
+    def __init__(self, owner, shape_points):
+        super().__init__(owner)
+        self.shape_points = shape_points
+
+    @staticmethod
+    def infer_dimensions(shape_points):
+        """Infer root chord and span from free-form points."""
+        down = False
+        for i in range(1, len(shape_points)):
+            if shape_points[i][1] > shape_points[i - 1][1] and down:
+                warnings.warn(
+                    "Jagged fin shape detected. This may cause small "
+                    "inaccuracies center of pressure and pitch moment "
+                    "calculations."
+                )
+                break
+            if shape_points[i][1] < shape_points[i - 1][1]:
+                down = True
+
+        root_chord = abs(shape_points[0][0] - shape_points[-1][0])
+        ys = [point[1] for point in shape_points]
+        span = max(ys) - min(ys)
+        return root_chord, span
+
+    def evaluate_geometrical_parameters(
+        self,
+    ):  # pylint: disable=too-many-statements,too-many-locals,invalid-name
+        """Calculate free-form fin geometric parameters."""
+        owner = self.owner
+
+        Af = 0
+        for i in range(len(self.shape_points) - 1):
+            x1, y1 = self.shape_points[i]
+            x2, y2 = self.shape_points[i + 1]
+            Af += (y1 + y2) * (x1 - x2)
+        Af = abs(Af) / 2
+        if Af < 1e-6:
+            raise ValueError("Fin area is too small. Check the shape_points.")
+
+        AR = 2 * owner.span**2 / Af
+        tau = (owner.span + owner.rocket_radius) / owner.rocket_radius
+        lift_interference_factor = 1 + 1 / tau
+
+        roll_forcing_interference_factor = (1 / np.pi**2) * (
+            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
+            + (np.pi * (tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
+            + ((tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
+            - (4 * (tau + 1))
+            / (tau * (tau - 1))
+            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
+        )
+
+        points_per_line = 40
+        chord_lead = np.ones(points_per_line) * np.inf
+        chord_trail = np.ones(points_per_line) * -np.inf
+        chord_length = np.zeros(points_per_line)
+
+        for p in range(1, len(self.shape_points)):
+            x1, y1 = self.shape_points[p - 1]
+            x2, y2 = self.shape_points[p]
+
+            prev_idx = int(y1 / owner.span * (points_per_line - 1))
+            curr_idx = int(y2 / owner.span * (points_per_line - 1))
+            prev_idx = np.clip(prev_idx, 0, points_per_line - 1)
+            curr_idx = np.clip(curr_idx, 0, points_per_line - 1)
+
+            if prev_idx > curr_idx:
+                prev_idx, curr_idx = curr_idx, prev_idx
+
+            for i in range(prev_idx, curr_idx + 1):
+                y = i * owner.span / (points_per_line - 1)
+                if y1 != y2:
+                    x = np.clip(
+                        (y - y2) / (y1 - y2) * x1 + (y1 - y) / (y1 - y2) * x2,
+                        min(x1, x2),
+                        max(x1, x2),
+                    )
+                else:
+                    x = x1
+
+                chord_lead[i] = min(chord_lead[i], x)
+                chord_trail[i] = max(chord_trail[i], x)
+
+                if y1 < y2:
+                    chord_length[i] -= x
+                else:
+                    chord_length[i] += x
+
+        invalid_lead = np.isnan(chord_lead) | np.isinf(chord_lead)
+        invalid_trail = np.isnan(chord_trail) | np.isinf(chord_trail)
+        chord_lead[invalid_lead | invalid_trail] = 0
+        chord_trail[invalid_lead | invalid_trail] = 0
+
+        chord_length[chord_length < 0] = 0
+        chord_length[np.isnan(chord_length)] = 0
+        max_chord = chord_trail - chord_lead
+        chord_length = np.minimum(chord_length, max_chord)
+
+        radius = owner.rocket_radius
+        total_area = 0
+        mac_length = 0
+        mac_lead = 0
+        mac_span = 0
+        cos_gamma_sum = 0
+        roll_geometrical_constant = 0
+        roll_damping_numerator = 0
+        roll_damping_denominator = 0
+
+        dy = owner.span / (points_per_line - 1)
+        for i in range(points_per_line):
+            chord = chord_trail[i] - chord_lead[i]
+            y = i * dy
+
+            mac_length += chord * chord
+            mac_span += y * chord
+            mac_lead += chord_lead[i] * chord
+            total_area += chord
+            roll_geometrical_constant += chord_length[i] * (radius + y) ** 2
+            roll_damping_numerator += radius**3 * chord / (radius + y) ** 2
+            roll_damping_denominator += (radius + y) * chord
+
+            if i > 0:
+                dx = (chord_trail[i] + chord_lead[i]) / 2 - (
+                    chord_trail[i - 1] + chord_lead[i - 1]
+                ) / 2
+                cos_gamma_sum += dy / np.hypot(dx, dy)
+
+        mac_length *= dy
+        mac_span *= dy
+        mac_lead *= dy
+        total_area *= dy
+        roll_geometrical_constant *= dy
+        roll_damping_numerator *= dy
+        roll_damping_denominator *= dy
+
+        mac_length /= total_area
+        mac_span /= total_area
+        mac_lead /= total_area
+        cos_gamma = cos_gamma_sum / (points_per_line - 1)
+
+        gamma_c = np.arccos(cos_gamma)
+
+        self.Af = Af
+        self.AR = AR
+        self.gamma_c = gamma_c
+        self.Yma = mac_span
+        self.mac_length = mac_length
+        self.mac_lead = mac_lead
+        self.tau = tau
+        self.roll_geometrical_constant = roll_geometrical_constant
+        self.lift_interference_factor = lift_interference_factor
+        self.roll_forcing_interference_factor = roll_forcing_interference_factor
+        self.roll_damping_interference_factor = 1 + (
+            roll_damping_numerator / roll_damping_denominator
+        )
+
+        return {
+            "Af": Af,
+            "AR": AR,
+            "gamma_c": gamma_c,
+            "Yma": mac_span,
+            "mac_length": mac_length,
+            "mac_lead": mac_lead,
+            "tau": tau,
+            "roll_geometrical_constant": roll_geometrical_constant,
+            "lift_interference_factor": lift_interference_factor,
+            "roll_forcing_interference_factor": roll_forcing_interference_factor,
+            "roll_damping_interference_factor": self.roll_damping_interference_factor,
+        }
+
+    def evaluate_shape(self):
+        x_array, y_array = zip(*self.shape_points)
+        shape_vec = [np.array(x_array), np.array(y_array)]
+        self.shape_vec = shape_vec
+        return shape_vec
+
+    def get_data(self, include_outputs=False):
+        data = {"shape_points": self.shape_points}
+        if include_outputs:
+            data.update(
+                {
+                    "Af": getattr(self, "Af", None),
+                    "AR": getattr(self, "AR", None),
+                    "gamma_c": getattr(self, "gamma_c", None),
+                    "Yma": getattr(self, "Yma", None),
+                    "mac_length": getattr(self, "mac_length", None),
+                    "mac_lead": getattr(self, "mac_lead", None),
+                    "roll_geometrical_constant": getattr(
+                        self, "roll_geometrical_constant", None
+                    ),
+                    "tau": getattr(self, "tau", None),
+                    "lift_interference_factor": getattr(
+                        self, "lift_interference_factor", None
+                    ),
+                    "roll_forcing_interference_factor": getattr(
+                        self, "roll_forcing_interference_factor", None
+                    ),
+                    "roll_damping_interference_factor": getattr(
+                        self, "roll_damping_interference_factor", None
+                    ),
+                }
+            )
+        return data
diff --git a/rocketpy/rocket/aero_surface/fins/elliptical_fin.py b/rocketpy/rocket/aero_surface/fins/elliptical_fin.py
new file mode 100644
index 000000000..66345f2cb
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/elliptical_fin.py
@@ -0,0 +1,196 @@
+from rocketpy.plots.aero_surface_plots import _EllipticalFinPlots
+from rocketpy.prints.aero_surface_prints import _EllipticalFinPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _EllipticalGeometry
+from rocketpy.rocket.aero_surface.fins.fin import Fin
+
+
+class EllipticalFin(Fin):
+    """Class that defines and holds information for an elliptical fin set.
+
+    This class inherits from the Fin class.
+
+    Note
+    ----
+    Local coordinate system:
+        - Origin located at the top of the root chord.
+        - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+        - Y axis perpendicular to the Z axis, in the span direction, positive upwards.
+        - X axis completes the right-handed coordinate system.
+
+    See Also
+    --------
+    Fin
+
+    Attributes
+    ----------
+    EllipticalFin.rocket_radius : float
+        The reference rocket radius used for lift coefficient normalization, in
+        meters.
+    EllipticalFin.airfoil : tuple
+        Tuple of two items. First is the airfoil lift curve.
+        Second is the unit of the curve (radians or degrees)
+    EllipticalFin.cant_angle : float
+        Fins cant angle with respect to the rocket centerline, in degrees.
+    EllipticalFin.cant_angle_rad : float
+        Fins cant angle with respect to the rocket centerline, in radians.
+    EllipticalFin.root_chord : float
+        Fin root chord in meters.
+    EllipticalFin.span : float
+        Fin span in meters.
+    EllipticalFin.name : string
+        Name of fin set.
+    EllipticalFin.sweep_length : float
+        Fins sweep length in meters. By sweep length, understand the axial
+        distance between the fin root leading edge and the fin tip leading edge
+        measured parallel to the rocket centerline.
+    EllipticalFin.sweep_angle : float
+        Fins sweep angle with respect to the rocket centerline. Must
+        be given in degrees.
+    EllipticalFin.rocket_diameter : float
+        Reference diameter of the rocket, in meters.
+    EllipticalFin.reference_area : float
+        Reference area of the rocket.
+    EllipticalFin.Af : float
+        Area of the longitudinal section of each fin in the set.
+    EllipticalFin.AR : float
+        Aspect ratio of the fin.
+    EllipticalFin.gamma_c : float
+        Fin mid-chord sweep angle.
+    EllipticalFin.Yma : float
+        Span wise position of the mean aerodynamic chord.
+    EllipticalFin.roll_geometrical_constant : float
+        Geometrical constant used in roll calculations.
+    EllipticalFin.tau : float
+        Geometrical relation used to simplify lift and roll calculations.
+    EllipticalFin.lift_interference_factor : float
+        Factor of Fin-Body interference in the lift coefficient.
+    EllipticalFin.cp : tuple
+        Tuple with the x, y and z local coordinates of the fin set center of
+        pressure. Has units of length and is given in meters.
+    EllipticalFin.cpx : float
+        Fin set local center of pressure x coordinate. Has units of length and
+        is given in meters.
+    EllipticalFin.cpy : float
+        Fin set local center of pressure y coordinate. Has units of length and
+        is given in meters.
+    EllipticalFin.cpz : float
+        Fin set local center of pressure z coordinate. Has units of length and
+        is given in meters.
+    EllipticalFin.cl : Function
+        Function which defines the lift coefficient as a function of the angle
+        of attack and the Mach number. Takes as input the angle of attack in
+        radians and the Mach number. Returns the lift coefficient.
+    EllipticalFin.clalpha : float
+        Lift coefficient slope. Has units of 1/rad.
+    """
+
+    def __init__(
+        self,
+        angular_position,
+        root_chord,
+        span,
+        rocket_radius,
+        cant_angle=0,
+        airfoil=None,
+        name="Elliptical Fin",
+    ):
+        """Initialize EllipticalFin class.
+
+        Parameters
+        ----------
+        angular_position : float
+            Angular position of the fin in degrees measured as the rotation
+            around the symmetry axis of the rocket relative to one of the other
+            principal axis. See :ref:`Angular Position Inputs <angular_position>`
+        root_chord : int, float
+            Fin root chord in meters.
+        span : int, float
+            Fin span in meters.
+        rocket_radius : int, float
+            Reference radius to calculate lift coefficient, in meters.
+        cant_angle : int, float, optional
+            Fins cant angle with respect to the rocket centerline. Must
+            be given in degrees.
+        sweep_length : int, float, optional
+            Fins sweep length in meters. By sweep length, understand the axial
+            distance between the fin root leading edge and the fin tip leading
+            edge measured parallel to the rocket centerline. If not given, the
+            sweep length is assumed to be equal the root chord minus the tip
+            chord, in which case the fin is a right trapezoid with its base
+            perpendicular to the rocket's axis. Cannot be used in conjunction
+            with sweep_angle.
+        sweep_angle : int, float, optional
+            Fins sweep angle with respect to the rocket centerline. Must
+            be given in degrees. If not given, the sweep angle is automatically
+            calculated, in which case the fin is assumed to be a right trapezoid
+            with its base perpendicular to the rocket's axis.
+            Cannot be used in conjunction with sweep_length.
+        airfoil : tuple, optional
+            Default is null, in which case fins will be treated as flat plates.
+            Otherwise, if tuple, fins will be considered as airfoils. The
+            tuple's first item specifies the airfoil's lift coefficient
+            by angle of attack and must be either a .csv, .txt, ndarray
+            or callable. The .csv and .txt files can contain a single line
+            header and the first column must specify the angle of attack, while
+            the second column must specify the lift coefficient. The
+            ndarray should be as [(x0, y0), (x1, y1), (x2, y2), ...]
+            where x0 is the angle of attack and y0 is the lift coefficient.
+            If callable, it should take an angle of attack as input and
+            return the lift coefficient at that angle of attack.
+            The tuple's second item is the unit of the angle of attack,
+            accepting either "radians" or "degrees".
+        name : str
+            Name of elliptical fin.
+
+        Returns
+        -------
+        None
+        """
+
+        super().__init__(
+            angular_position,
+            root_chord,
+            span,
+            rocket_radius,
+            cant_angle,
+            airfoil,
+            name,
+        )
+
+        self.geometry = _EllipticalGeometry(self)
+        self._update_geometry_chain()
+        self.evaluate_shape()
+        self.evaluate_rotation_matrix()
+
+        self.prints = _EllipticalFinPrints(self)
+        self.plots = _EllipticalFinPlots(self)
+
+    def evaluate_center_of_pressure(self):
+        """Calculates and returns the center of pressure of the fin in local
+        coordinates. The center of pressure position is saved and stored as a
+        tuple."""
+        # Barrowman elliptical-fin center of pressure location.
+        cpz = 0.288 * self.root_chord
+        self.cpx = 0
+        self.cpy = self.Yma
+        self.cpz = cpz
+        self.cp = (self.cpx, self.cpy, self.cpz)
+
+    def to_dict(self, **kwargs):
+        data = super().to_dict(**kwargs)
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
+        return data
+
+    @classmethod
+    def from_dict(cls, data):
+        return cls(
+            angular_position=data["angular_position"],
+            root_chord=data["root_chord"],
+            span=data["span"],
+            rocket_radius=data["rocket_radius"],
+            cant_angle=data["cant_angle"],
+            airfoil=data["airfoil"],
+            name=data["name"],
+        )
diff --git a/rocketpy/rocket/aero_surface/fins/elliptical_fins.py b/rocketpy/rocket/aero_surface/fins/elliptical_fins.py
index 61d98bc0d..4576bd1f3 100644
--- a/rocketpy/rocket/aero_surface/fins/elliptical_fins.py
+++ b/rocketpy/rocket/aero_surface/fins/elliptical_fins.py
@@ -1,7 +1,6 @@
-import numpy as np
-
 from rocketpy.plots.aero_surface_plots import _EllipticalFinsPlots
 from rocketpy.prints.aero_surface_prints import _EllipticalFinsPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _EllipticalGeometry
 
 from .fins import Fins
 
@@ -35,9 +34,6 @@ class EllipticalFins(Fins):
         Second is the unit of the curve (radians or degrees)
     EllipticalFins.cant_angle : float
         Fins cant angle with respect to the rocket centerline, in degrees.
-    EllipticalFins.changing_attribute_dict : dict
-        Dictionary that stores the name and the values of the attributes that
-        may be changed during a simulation. Useful for control systems.
     EllipticalFins.cant_angle_rad : float
         Fins cant angle with respect to the rocket centerline, in radians.
     EllipticalFins.root_chord : float
@@ -53,9 +49,9 @@ class EllipticalFins(Fins):
     EllipticalFins.sweep_angle : float
         Fins sweep angle with respect to the rocket centerline. Must
         be given in degrees.
-    EllipticalFins.d : float
+    EllipticalFins.rocket_diameter : float
         Reference diameter of the rocket, in meters.
-    EllipticalFins.ref_area : float
+    EllipticalFins.reference_area : float
         Reference area of the rocket.
     EllipticalFins.Af : float
         Area of the longitudinal section of each fin in the set.
@@ -162,10 +158,9 @@ def __init__(
             name,
         )
 
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry = _EllipticalGeometry(self)
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
         self.prints = _EllipticalFinsPrints(self)
         self.plots = _EllipticalFinsPlots(self)
@@ -179,160 +174,18 @@ def evaluate_center_of_pressure(self):
         -------
         None
         """
-        # Center of pressure position in local coordinates
+        # Barrowman elliptical-fin center of pressure location.
         cpz = 0.288 * self.root_chord
         self.cpx = 0
         self.cpy = 0
         self.cpz = cpz
         self.cp = (self.cpx, self.cpy, self.cpz)
 
-    def evaluate_geometrical_parameters(self):  # pylint: disable=too-many-statements
-        """Calculates and saves fin set's geometrical parameters such as the
-        fins' area, aspect ratio and parameters for roll movement.
-
-        Returns
-        -------
-        None
-        """
-
-        # Compute auxiliary geometrical parameters
-        # pylint: disable=invalid-name
-        Af = (np.pi * self.root_chord / 2 * self.span) / 2  # Fin area
-        gamma_c = 0  # Zero for elliptical fins
-        AR = 2 * self.span**2 / Af  # Fin aspect ratio
-        Yma = (
-            self.span / (3 * np.pi) * np.sqrt(9 * np.pi**2 - 64)
-        )  # Span wise coord of mean aero chord
-        roll_geometrical_constant = (
-            self.root_chord
-            * self.span
-            * (
-                3 * np.pi * self.span**2
-                + 32 * self.rocket_radius * self.span
-                + 12 * np.pi * self.rocket_radius**2
-            )
-            / 48
-        )
-
-        # Fin–body interference correction parameters
-        tau = (self.span + self.rocket_radius) / self.rocket_radius
-        lift_interference_factor = 1 + 1 / tau
-        if self.span > self.rocket_radius:
-            roll_damping_interference_factor = 1 + (
-                (self.rocket_radius**2)
-                * (
-                    2
-                    * (self.rocket_radius**2)
-                    * np.sqrt(self.span**2 - self.rocket_radius**2)
-                    * np.log(
-                        (
-                            2
-                            * self.span
-                            * np.sqrt(self.span**2 - self.rocket_radius**2)
-                            + 2 * self.span**2
-                        )
-                        / self.rocket_radius
-                    )
-                    - 2
-                    * (self.rocket_radius**2)
-                    * np.sqrt(self.span**2 - self.rocket_radius**2)
-                    * np.log(2 * self.span)
-                    + 2 * self.span**3
-                    - np.pi * self.rocket_radius * self.span**2
-                    - 2 * (self.rocket_radius**2) * self.span
-                    + np.pi * self.rocket_radius**3
-                )
-            ) / (
-                2
-                * (self.span**2)
-                * (self.span / 3 + np.pi * self.rocket_radius / 4)
-                * (self.span**2 - self.rocket_radius**2)
-            )
-        elif self.span < self.rocket_radius:
-            roll_damping_interference_factor = 1 - (
-                self.rocket_radius**2
-                * (
-                    2 * self.span**3
-                    - np.pi * self.span**2 * self.rocket_radius
-                    - 2 * self.span * self.rocket_radius**2
-                    + np.pi * self.rocket_radius**3
-                    + 2
-                    * self.rocket_radius**2
-                    * np.sqrt(-(self.span**2) + self.rocket_radius**2)
-                    * np.arctan(
-                        (self.span) / (np.sqrt(-(self.span**2) + self.rocket_radius**2))
-                    )
-                    - np.pi
-                    * self.rocket_radius**2
-                    * np.sqrt(-(self.span**2) + self.rocket_radius**2)
-                )
-            ) / (
-                2
-                * self.span
-                * (-(self.span**2) + self.rocket_radius**2)
-                * (self.span**2 / 3 + np.pi * self.span * self.rocket_radius / 4)
-            )
-        else:
-            roll_damping_interference_factor = (28 - 3 * np.pi) / (4 + 3 * np.pi)
-
-        roll_forcing_interference_factor = (1 / np.pi**2) * (
-            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
-            + ((np.pi * (tau**2 + 1) ** 2) / (tau**2 * (tau - 1) ** 2))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
-            + ((tau**2 + 1) ** 2)
-            / (tau**2 * (tau - 1) ** 2)
-            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
-            - (4 * (tau + 1))
-            / (tau * (tau - 1))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
-        )
-
-        # Store values
-        # pylint: disable=invalid-name
-        self.Af = Af  # Fin area
-        self.AR = AR  # Fin aspect ratio
-        self.gamma_c = gamma_c  # Mid chord angle
-        self.Yma = Yma  # Span wise coord of mean aero chord
-        self.roll_geometrical_constant = roll_geometrical_constant
-        self.tau = tau
-        self.lift_interference_factor = lift_interference_factor
-        self.roll_damping_interference_factor = roll_damping_interference_factor
-        self.roll_forcing_interference_factor = roll_forcing_interference_factor
-
-        self.evaluate_shape()
-
-    def evaluate_shape(self):
-        angles = np.arange(0, 180, 5)
-        x_array = self.root_chord / 2 + self.root_chord / 2 * np.cos(np.radians(angles))
-        y_array = self.span * np.sin(np.radians(angles))
-        self.shape_vec = [x_array, y_array]
-
-    def info(self):
-        self.prints.geometry()
-        self.prints.lift()
-
-    def all_info(self):
-        self.prints.all()
-        self.plots.all()
-
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
-        if kwargs.get("include_outputs", False):
-            data.update(
-                {
-                    "Af": self.Af,
-                    "AR": self.AR,
-                    "gamma_c": self.gamma_c,
-                    "Yma": self.Yma,
-                    "roll_geometrical_constant": self.roll_geometrical_constant,
-                    "tau": self.tau,
-                    "lift_interference_factor": self.lift_interference_factor,
-                    "roll_damping_interference_factor": self.roll_damping_interference_factor,
-                    "roll_forcing_interference_factor": self.roll_forcing_interference_factor,
-                }
-            )
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
         return data
 
     @classmethod
diff --git a/rocketpy/rocket/aero_surface/fins/fin.py b/rocketpy/rocket/aero_surface/fins/fin.py
new file mode 100644
index 000000000..bb41c89d2
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/fin.py
@@ -0,0 +1,483 @@
+import math
+
+import numpy as np
+
+from rocketpy.mathutils.function import Function
+from rocketpy.mathutils.vector_matrix import Matrix, Vector
+from rocketpy.rocket.aero_surface.fins._base_fin import _BaseFin
+
+
+class Fin(_BaseFin):
+    """Abstract class that holds common methods for the individual fin classes.
+    Cannot be instantiated.
+
+    Note
+    ----
+    Local coordinate system:
+        - Origin located at the top of the root chord.
+        - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+        - Y axis perpendicular to the Z axis, in the span direction, positive upwards.
+        - X axis completes the right-handed coordinate system.
+
+    Attributes
+    ----------
+    Fin.rocket_radius : float
+        The reference rocket radius used for lift coefficient normalization,
+        in meters.
+    Fin.airfoil : tuple
+        Tuple of two items. First is the airfoil lift curve.
+        Second is the unit of the curve (radians or degrees).
+    Fin.cant_angle : float
+        Fin cant angle with respect to the rocket centerline, in degrees.
+    Fin.changing_attribute_dict : dict
+        Dictionary that stores the name and the values of the attributes that
+        may be changed during a simulation. Useful for control systems.
+    Fin.cant_angle_rad : float
+        Fin cant angle with respect to the rocket centerline, in radians.
+    Fin.root_chord : float
+        Fin root chord in meters.
+    Fin.tip_chord : float
+        Fin tip chord in meters.
+    Fin.span : float
+        Fin span in meters.
+    Fin.name : string
+        Name of fin set.
+    Fin.sweep_length : float
+        Fin sweep length in meters. By sweep length, understand the axial
+        distance between the fin root leading edge and the fin tip leading edge
+        measured parallel to the rocket centerline.
+    Fin.sweep_angle : float
+        Fin sweep angle with respect to the rocket centerline. Must
+        be given in degrees.
+    Fin.rocket_diameter : float
+        Reference diameter of the rocket. Has units of length and is given
+        in meters.
+    Fin.reference_area : float
+        Reference area of the rocket.
+    Fin.Af : float
+        Area of the longitudinal section of each fin in the set.
+    Fin.AR : float
+        Aspect ratio of each fin in the set.
+    Fin.gamma_c : float
+        Fin mid-chord sweep angle.
+    Fin.Yma : float
+        Span wise position of the mean aerodynamic chord.
+    Fin.roll_geometrical_constant : float
+        Geometrical constant used in roll calculations.
+    Fin.tau : float
+        Geometrical relation used to simplify lift and roll calculations.
+    Fin.lift_interference_factor : float
+        Factor of Fin-Body interference in the lift coefficient.
+    Fin.cp : tuple
+        Tuple with the x, y and z local coordinates of the fin set center of
+        pressure. Has units of length and is given in meters.
+    Fin.cpx : float
+        Fin set local center of pressure x coordinate. Has units of length and
+        is given in meters.
+    Fin.cpy : float
+        Fin set local center of pressure y coordinate. Has units of length and
+        is given in meters.
+    Fin.cpz : float
+        Fin set local center of pressure z coordinate. Has units of length and
+        is given in meters.
+    Fin.cl : Function
+        Function which defines the lift coefficient as a function of the angle
+        of attack and the Mach number. Takes as input the angle of attack in
+        radians and the Mach number. Returns the lift coefficient.
+    Fin.clalpha : float
+        Lift coefficient slope. Has units of 1/rad.
+    Fin.roll_parameters : list
+        List containing the roll moment lift coefficient, the roll moment
+        damping coefficient and the cant angle in radians.
+    """
+
+    def __init__(
+        self,
+        angular_position,
+        root_chord,
+        span,
+        rocket_radius,
+        cant_angle=0,
+        airfoil=None,
+        name="Fin",
+    ):
+        """Initialize Fin class.
+
+        Parameters
+        ----------
+        angular_position : float
+            Angular position of the fin in degrees measured as the rotation
+            around the symmetry axis of the rocket relative to one of the other
+            principal axis. See :ref:`Angular Position Inputs <angular_position>`
+        root_chord : int, float
+            Fin root chord in meters.
+        span : int, float
+            Fin span in meters.
+        rocket_radius : int, float
+            Reference rocket radius used for lift coefficient normalization.
+        cant_angle : int, float, optional
+            Fin cant angle with respect to the rocket centerline. Must
+            be given in degrees.
+        airfoil : tuple, optional
+            Default is null, in which case fins will be treated as flat plates.
+            Otherwise, if tuple, fins will be considered as airfoils. The
+            tuple's first item specifies the airfoil's lift coefficient
+            by angle of attack and must be either a .csv, .txt, ndarray
+            or callable. The .csv and .txt files can contain a single line
+            header and the first column must specify the angle of attack, while
+            the second column must specify the lift coefficient. The
+            ndarray should be as [(x0, y0), (x1, y1), (x2, y2), ...]
+            where x0 is the angle of attack and y0 is the lift coefficient.
+            If callable, it should take an angle of attack as input and
+            return the lift coefficient at that angle of attack.
+            The tuple's second item is the unit of the angle of attack,
+            accepting either "radians" or "degrees".
+        name : str
+            Name of fin.
+        """
+        super().__init__(
+            name=name,
+            rocket_radius=rocket_radius,
+            root_chord=root_chord,
+            span=span,
+            airfoil=airfoil,
+            cant_angle=cant_angle,
+        )
+
+        # Store values
+        self._angular_position = angular_position
+        self._angular_position_rad = math.radians(angular_position)
+
+    @property
+    def cant_angle(self):
+        return self._cant_angle
+
+    @cant_angle.setter
+    def cant_angle(self, value):
+        self._cant_angle = value
+        self.cant_angle_rad = math.radians(value)
+
+    @property
+    def cant_angle_rad(self):
+        return self._cant_angle_rad
+
+    @cant_angle_rad.setter
+    def cant_angle_rad(self, value):
+        self._cant_angle_rad = value
+        self.evaluate_geometrical_parameters()
+        self.evaluate_center_of_pressure()
+        self.evaluate_lift_coefficient()
+        self.evaluate_roll_parameters()
+        self.evaluate_rotation_matrix()
+
+    @property
+    def angular_position(self):
+        return self._angular_position
+
+    @angular_position.setter
+    def angular_position(self, value):
+        self._angular_position = value
+        self.angular_position_rad = math.radians(value)
+
+    @property
+    def angular_position_rad(self):
+        return self._angular_position_rad
+
+    @angular_position_rad.setter
+    def angular_position_rad(self, value):
+        self._angular_position_rad = value
+        self.evaluate_rotation_matrix()
+
+    def evaluate_lift_coefficient(self):
+        """Calculates and returns the individual fin's lift coefficient.
+
+        Note
+        ----
+        An individual :class:`Fin` models a single physical fin, so its lift
+        curve slope is the single-fin value corrected only for fin-body
+        interference. It intentionally does NOT include the empirical
+        multiple-fin interference correction (``fin_num_correction``) applied by
+        the symmetric :class:`Fins` set, because that correction is defined for a
+        set of ``n`` identical, evenly spaced fins and has no meaning for an
+        individually positioned fin. Consequently, a set of ``n`` identical
+        ``Fin`` objects will not reproduce the exact aggregate lift slope of a
+        ``Fins(n=...)`` set (they differ by ``fin_num_correction(n) / n``). For
+        standard symmetric fin sets, prefer the plural ``*Fins`` classes.
+
+        Returns
+        -------
+        None
+        """
+        self.evaluate_single_fin_lift_coefficient()
+
+        self.clalpha = self.clalpha_single_fin * self.lift_interference_factor
+
+        # Cl = clalpha * alpha
+        self.cl = Function(
+            lambda alpha, mach: alpha * self.clalpha(mach),
+            ["Alpha (rad)", "Mach"],
+            "Lift coefficient",
+        )
+
+        return self.cl
+
+    def evaluate_roll_parameters(self):
+        """Calculates and returns the fin set's roll coefficients.
+        The roll coefficients are saved in a list.
+
+        Returns
+        -------
+        self.roll_parameters : list
+            List containing the roll moment lift coefficient, the
+            roll moment damping coefficient and the cant angle in
+            radians
+        """
+        clf_delta = (
+            self.roll_forcing_interference_factor
+            * (self.Yma + self.rocket_radius)
+            * self.clalpha_single_fin
+            / self.reference_length
+        )  # Function of mach number
+        clf_delta.set_inputs("Mach")
+        clf_delta.set_outputs("Roll moment forcing coefficient derivative")
+        clf_delta.set_title(
+            "Roll moment forcing coefficient derivative vs. Mach number"
+        )
+        cld_omega = -(
+            2
+            * self.roll_damping_interference_factor
+            * self.clalpha_single_fin
+            * np.cos(self.cant_angle_rad)
+            * self.roll_geometrical_constant
+            / (self.reference_area * self.reference_length**2)
+        )  # Function of mach number
+        cld_omega.set_inputs("Mach")
+        cld_omega.set_outputs("Roll moment damping coefficient derivative")
+        cld_omega.set_title(
+            "Roll moment damping coefficient derivative vs. Mach number"
+        )
+        self.roll_parameters = [clf_delta, cld_omega, self.cant_angle_rad]
+        return self.roll_parameters
+
+    def evaluate_rotation_matrix(self):
+        """Calculates and returns the rotation matrix from the rocket body frame
+        to the fin frame.
+
+        Note
+        ----
+        Local coordinate system:
+
+        - Origin located at the leading edge of the root chord.
+        - Z axis along the longitudinal axis of the fin, positive
+          downwards (leading edge -> trailing edge).
+        - Y axis perpendicular to the Z axis, in the span direction,
+          positive upwards (root chord -> tip chord).
+        - X axis completes the right-handed coordinate system.
+
+
+        Returns
+        -------
+        None
+
+        References
+        ----------
+        :ref:`Individual Fin Model <individual_fins>`
+        """
+        phi = self.angular_position_rad
+        delta = self.cant_angle_rad
+        sin_phi = math.sin(phi)
+        cos_phi = math.cos(phi)
+        sin_delta = math.sin(delta)
+        cos_delta = math.cos(delta)
+
+        # Rotation about body Z by angular position
+        R_phi = Matrix(
+            [
+                [cos_phi, -sin_phi, 0],
+                [sin_phi, cos_phi, 0],
+                [0, 0, 1],
+            ]
+        )
+
+        # Cant rotation about body Y
+        R_delta = Matrix(
+            [
+                [cos_delta, 0, -sin_delta],
+                [0, 1, 0],
+                [sin_delta, 0, cos_delta],
+            ]
+        )
+
+        # 180 flip about Y to align fin leading/trailing edge
+        R_pi = Matrix(
+            [
+                [-1, 0, 0],
+                [0, 1, 0],
+                [0, 0, -1],
+            ]
+        )
+
+        # Uncanted body to fin, then apply cant
+        R_uncanted = R_phi @ R_pi
+        R_body_to_fin = R_delta @ R_uncanted
+
+        # Store for downstream transforms
+        self._rotation_fin_to_body_uncanted = R_uncanted.transpose
+        self._rotation_body_to_fin = R_body_to_fin
+        self._rotation_fin_to_body = R_body_to_fin.transpose
+        self._rotation_surface_to_body = self._rotation_fin_to_body
+
+    def compute_forces_and_moments(
+        self,
+        stream_velocity,
+        stream_speed,
+        stream_mach,
+        rho,
+        cp,
+        omega,
+        *args,
+    ):  # pylint: disable=arguments-differ,unused-argument
+        """Computes the forces and moments acting on the aerodynamic surface.
+
+        Parameters
+        ----------
+        stream_velocity : tuple of float
+            The velocity of the airflow relative to the surface.
+        stream_speed : float
+            The magnitude of the airflow speed.
+        stream_mach : float
+            The Mach number of the airflow.
+        rho : float
+            Air density.
+        cp : Vector
+            Center of pressure coordinates in the body frame.
+        omega: tuple[float, float, float]
+            Tuple containing angular velocities around the x, y, z axes.
+
+        Returns
+        -------
+        tuple of float
+            The aerodynamic forces (lift, side_force, drag) and moments
+            (pitch, yaw, roll) in the body frame.
+        """
+        R1, R2, R3, M1, M2, M3 = 0, 0, 0, 0, 0, 0
+
+        # stream velocity in fin frame
+        stream_velocity_f = self._rotation_body_to_fin @ stream_velocity
+
+        attack_angle = np.arctan2(stream_velocity_f[0], stream_velocity_f[2])
+        # Force in the X direction of the fin
+        X = (
+            0.5
+            * rho
+            * stream_speed**2
+            * self.reference_area
+            * self.cl.get_value_opt(attack_angle, stream_mach)
+        )
+        # Force in body frame
+        R1, R2, R3 = self._rotation_fin_to_body @ Vector([X, 0, 0])
+        # Moments
+        M1, M2, M3 = cp ^ Vector([R1, R2, R3])
+        # Apply roll interference factor, disregarding lift interference factor
+        M3 *= self.roll_forcing_interference_factor / self.lift_interference_factor
+
+        # NOTE: roll damping is intentionally NOT added as a separate term here.
+        # Unlike the symmetric fin set (whose center of pressure lies on the
+        # roll axis), an individual fin has an off-axis center of pressure, so
+        # the roll-rate contribution ``w ^ cp`` is already injected by the Flight
+        # loop into the local stream velocity fed to this surface (see
+        # ``Flight`` ``comp_vb``). That contribution changes ``attack_angle`` and
+        # therefore already produces the roll-damping moment through the
+        # ``cp ^ R`` term above. Adding an explicit ``cld_omega`` damping term
+        # would double-count it.
+        return R1, R2, R3, M1, M2, M3
+
+    def _compute_leading_edge_position(self, position, _csys):
+        """Computes the position of the fin leading edge in a rocket's user,
+        given its position in a rocket."""
+        # Point from deflection from cant angle in the plane perpendicular to
+        # the fuselage where the fin is located in the fin frame
+        p = Vector(
+            [
+                -self.root_chord / 2 * np.sin(self.cant_angle_rad),
+                0,
+                self.root_chord / 2 * (1 - np.cos(self.cant_angle_rad)),
+            ]
+        )
+        # Rotate the point to the body frame orientation
+        p = self._rotation_fin_to_body_uncanted @ p
+
+        # Rotate the point to the user-defined coordinate system
+        p = Vector([p.x * _csys, p.y, p.z * _csys])
+
+        # Build the leading-edge position in the user frame as if no cant
+        # angle was applied. Scalars are interpreted as z coordinates only,
+        # while vectors/tuples/lists are interpreted as full (x, y, z)
+        # coordinates.
+        if isinstance(position, (Vector, tuple, list)):
+            position = Vector(position)
+        else:
+            position = Vector(
+                [
+                    -self.rocket_radius * math.sin(self.angular_position_rad) * _csys,
+                    self.rocket_radius * math.cos(self.angular_position_rad),
+                    position,
+                ]
+            )
+
+        # Translate the position of the fin leading edge to the position of the
+        # fin leading edge with cant angle
+        position += p
+        return position
+
+    def to_dict(self, **kwargs):
+        if self.airfoil:
+            if kwargs.get("discretize", False):
+                lower = -np.pi / 6 if self.airfoil[1] == "radians" else -30
+                upper = np.pi / 6 if self.airfoil[1] == "radians" else 30
+                airfoil = (
+                    self.airfoil_cl.set_discrete(lower, upper, 50, mutate_self=False),
+                    self.airfoil[1],
+                )
+            else:
+                airfoil = (self.airfoil_cl, self.airfoil[1])
+        else:
+            airfoil = None
+        data = {
+            "angular_position": self.angular_position,
+            "root_chord": self.root_chord,
+            "span": self.span,
+            "rocket_radius": self.rocket_radius,
+            "cant_angle": self.cant_angle,
+            "airfoil": airfoil,
+            "name": self.name,
+        }
+
+        if kwargs.get("include_outputs", False):
+            data.update(
+                {
+                    "cp": self.cp,
+                    "cl": self.cl,
+                    "roll_parameters": self.roll_parameters,
+                    "rocket_diameter": self.rocket_diameter,
+                    "diameter": self.rocket_diameter,
+                    "d": self.rocket_diameter,
+                    "reference_area": self.reference_area,
+                    "ref_area": self.reference_area,
+                }
+            )
+        return data
+
+    def draw(self, *, filename=None):
+        """Draw the fin shape along with some important information, including
+        the center line, the quarter line and the center of pressure position.
+
+        Parameters
+        ----------
+        filename : str | None, optional
+            The path the plot should be saved to. By default None, in which case
+            the plot will be shown instead of saved. Supported file endings are:
+            eps, jpg, jpeg, pdf, pgf, png, ps, raw, rgba, svg, svgz, tif, tiff
+            and webp (these are the formats supported by matplotlib).
+        """
+        self.plots.draw(filename=filename)
diff --git a/rocketpy/rocket/aero_surface/fins/fins.py b/rocketpy/rocket/aero_surface/fins/fins.py
index fe24a84f4..912212979 100644
--- a/rocketpy/rocket/aero_surface/fins/fins.py
+++ b/rocketpy/rocket/aero_surface/fins/fins.py
@@ -1,11 +1,10 @@
 import numpy as np
 
 from rocketpy.mathutils.function import Function
+from rocketpy.rocket.aero_surface.fins._base_fin import _BaseFin
 
-from ..aero_surface import AeroSurface
 
-
-class Fins(AeroSurface):
+class Fins(_BaseFin):
     """Abstract class that holds common methods for the fin classes.
     Cannot be instantiated.
 
@@ -49,10 +48,10 @@ class Fins(AeroSurface):
     Fins.sweep_angle : float
         Fins sweep angle with respect to the rocket centerline. Must
         be given in degrees.
-    Fins.d : float
+    Fins.rocket_diameter : float
         Reference diameter of the rocket. Has units of length and is given
         in meters.
-    Fins.ref_area : float
+    Fins.reference_area : float
         Reference area of the rocket.
     Fins.Af : float
         Area of the longitudinal section of each fin in the set.
@@ -132,27 +131,18 @@ def __init__(
             accepting either "radians" or "degrees".
         name : str
             Name of fin set.
-
-        Returns
-        -------
-        None
         """
-        # Compute auxiliary geometrical parameters
-        d = 2 * rocket_radius
-        ref_area = np.pi * rocket_radius**2  # Reference area
-
-        super().__init__(name, ref_area, d)
+        super().__init__(
+            name=name,
+            rocket_radius=rocket_radius,
+            root_chord=root_chord,
+            span=span,
+            airfoil=airfoil,
+            cant_angle=cant_angle,
+        )
 
         # Store values
         self._n = n
-        self._rocket_radius = rocket_radius
-        self._airfoil = airfoil
-        self._cant_angle = cant_angle
-        self._root_chord = root_chord
-        self._span = span
-        self.name = name
-        self.d = d
-        self.ref_area = ref_area  # Reference area
 
     @property
     def n(self):
@@ -166,134 +156,26 @@ def n(self, value):
         self.evaluate_lift_coefficient()
         self.evaluate_roll_parameters()
 
-    @property
-    def root_chord(self):
-        return self._root_chord
-
-    @root_chord.setter
-    def root_chord(self, value):
-        self._root_chord = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
-
-    @property
-    def span(self):
-        return self._span
-
-    @span.setter
-    def span(self, value):
-        self._span = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
-
-    @property
-    def rocket_radius(self):
-        return self._rocket_radius
-
-    @rocket_radius.setter
-    def rocket_radius(self, value):
-        self._rocket_radius = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
-
-    @property
-    def cant_angle(self):
-        return self._cant_angle
-
-    @cant_angle.setter
-    def cant_angle(self, value):
-        self._cant_angle = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
-
-    @property
-    def airfoil(self):
-        return self._airfoil
-
-    @airfoil.setter
-    def airfoil(self, value):
-        self._airfoil = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
-
     def evaluate_lift_coefficient(self):
         """Calculates and returns the fin set's lift coefficient.
         The lift coefficient is saved and returned. This function
         also calculates and saves the lift coefficient derivative
         for a single fin and the lift coefficient derivative for
         a number of n fins corrected for Fin-Body interference.
-
-        Returns
-        -------
-        None
         """
-        if not self.airfoil:
-            # Defines clalpha2D as 2*pi for planar fins
-            clalpha2D_incompressible = 2 * np.pi
-        else:
-            # Defines clalpha2D as the derivative of the lift coefficient curve
-            # for the specific airfoil
-            self.airfoil_cl = Function(
-                self.airfoil[0],
-                interpolation="linear",
-            )
-
-            # Differentiating at alpha = 0 to get cl_alpha
-            clalpha2D_incompressible = self.airfoil_cl.differentiate_complex_step(
-                x=1e-3, dx=1e-3
-            )
-
-            # Convert to radians if needed
-            if self.airfoil[1] == "degrees":
-                clalpha2D_incompressible *= 180 / np.pi
-
-        # Correcting for compressible flow (apply Prandtl-Glauert correction)
-        clalpha2D = Function(lambda mach: clalpha2D_incompressible / self._beta(mach))
-
-        # Diederich's Planform Correlation Parameter
-        planform_correlation_parameter = (
-            2 * np.pi * self.AR / (clalpha2D * np.cos(self.gamma_c))
-        )
-
-        # Lift coefficient derivative for a single fin
-        def lift_source(mach):
-            return (
-                clalpha2D(mach)
-                * planform_correlation_parameter(mach)
-                * (self.Af / self.ref_area)
-                * np.cos(self.gamma_c)
-            ) / (
-                2
-                + planform_correlation_parameter(mach)
-                * np.sqrt(1 + (2 / planform_correlation_parameter(mach)) ** 2)
-            )
-
-        self.clalpha_single_fin = Function(
-            lift_source,
-            "Mach",
-            "Lift coefficient derivative for a single fin",
-        )
+        self.evaluate_single_fin_lift_coefficient()
 
         # Lift coefficient derivative for n fins corrected with Fin-Body interference
         self.clalpha_multiple_fins = (
-            self.lift_interference_factor
-            * self.fin_num_correction(self.n)
+            self.fin_num_correction(self.n)
+            * self.lift_interference_factor
             * self.clalpha_single_fin
         )  # Function of mach number
         self.clalpha_multiple_fins.set_inputs("Mach")
         self.clalpha_multiple_fins.set_outputs(
             f"Lift coefficient derivative for {self.n:.0f} fins"
         )
+
         self.clalpha = self.clalpha_multiple_fins
 
         # Cl = clalpha * alpha
@@ -316,19 +198,18 @@ def evaluate_roll_parameters(self):
             roll moment damping coefficient and the cant angle in
             radians
         """
-
-        self.cant_angle_rad = np.radians(self.cant_angle)
-
         clf_delta = (
             self.roll_forcing_interference_factor
             * self.n
             * (self.Yma + self.rocket_radius)
             * self.clalpha_single_fin
-            / self.d
+            / self.reference_length
         )  # Function of mach number
         clf_delta.set_inputs("Mach")
         clf_delta.set_outputs("Roll moment forcing coefficient derivative")
-        clf_delta.set_title(None)
+        clf_delta.set_title(
+            "Roll moment forcing coefficient derivative vs. Mach number"
+        )
         cld_omega = (
             2
             * self.roll_damping_interference_factor
@@ -336,11 +217,13 @@ def evaluate_roll_parameters(self):
             * self.clalpha_single_fin
             * np.cos(self.cant_angle_rad)
             * self.roll_geometrical_constant
-            / (self.ref_area * self.d**2)
+            / (self.reference_area * self.reference_length**2)
         )  # Function of mach number
         cld_omega.set_inputs("Mach")
         cld_omega.set_outputs("Roll moment damping coefficient derivative")
-        cld_omega.set_title(None)
+        cld_omega.set_title(
+            "Roll moment damping coefficient derivative vs. Mach number"
+        )
         self.roll_parameters = [clf_delta, cld_omega, self.cant_angle_rad]
         return self.roll_parameters
 
@@ -463,8 +346,11 @@ def to_dict(self, **kwargs):
                     "cp": self.cp,
                     "cl": cl,
                     "roll_parameters": self.roll_parameters,
-                    "d": self.d,
-                    "ref_area": self.ref_area,
+                    "rocket_diameter": self.rocket_diameter,
+                    "diameter": self.rocket_diameter,
+                    "d": self.rocket_diameter,
+                    "reference_area": self.reference_area,
+                    "ref_area": self.reference_area,
                 }
             )
 
@@ -481,9 +367,5 @@ def draw(self, *, filename=None):
             the plot will be shown instead of saved. Supported file endings are:
             eps, jpg, jpeg, pdf, pgf, png, ps, raw, rgba, svg, svgz, tif, tiff
             and webp (these are the formats supported by matplotlib).
-
-        Returns
-        -------
-        None
         """
         self.plots.draw(filename=filename)
diff --git a/rocketpy/rocket/aero_surface/fins/free_form_fin.py b/rocketpy/rocket/aero_surface/fins/free_form_fin.py
new file mode 100644
index 000000000..767b1bd89
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/free_form_fin.py
@@ -0,0 +1,192 @@
+from rocketpy.plots.aero_surface_plots import _FreeFormFinPlots
+from rocketpy.prints.aero_surface_prints import _FreeFormFinPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _FreeFormGeometry
+from rocketpy.rocket.aero_surface.fins.fin import Fin
+
+
+class FreeFormFin(Fin):
+    """Class that defines and holds information for a free form fin set.
+
+    This class inherits from the Fin class.
+
+    Note
+    ----
+    Local coordinate system:
+        - Origin located at the top of the root chord.
+        - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+        - Y axis perpendicular to the Z axis, in the span direction, positive upwards.
+        - X axis completes the right-handed coordinate system.
+
+    See Also
+    --------
+    Fin
+
+    Attributes
+    ----------
+    FreeFormFin.n : int
+        Number of fins in fin set.
+    FreeFormFin.rocket_radius : float
+        The reference rocket radius used for lift coefficient normalization, in
+        meters.
+    FreeFormFin.airfoil : tuple
+        Tuple of two items. First is the airfoil lift curve.
+        Second is the unit of the curve (radians or degrees).
+    FreeFormFin.cant_angle : float
+        Fins cant angle with respect to the rocket centerline, in degrees.
+    FreeFormFin.cant_angle_rad : float
+        Fins cant angle with respect to the rocket centerline, in radians.
+    FreeFormFin.root_chord : float
+        Fin root chord in meters.
+    FreeFormFin.span : float
+        Fin span in meters.
+    FreeFormFin.name : string
+        Name of fin set.
+    FreeFormFin.rocket_diameter : float
+        Reference diameter of the rocket, in meters.
+    FreeFormFin.reference_area : float
+        Reference area of the rocket, in m².
+    FreeFormFin.Af : float
+        Area of the longitudinal section of each fin in the set.
+    FreeFormFin.AR : float
+        Aspect ratio of the fin.
+    FreeFormFin.gamma_c : float
+        Fin mid-chord sweep angle.
+    FreeFormFin.Yma : float
+        Span wise position of the mean aerodynamic chord.
+    FreeFormFin.roll_geometrical_constant : float
+        Geometrical constant used in roll calculations.
+    FreeFormFin.tau : float
+        Geometrical relation used to simplify lift and roll calculations.
+    FreeFormFin.lift_interference_factor : float
+        Factor of Fin-Body interference in the lift coefficient.
+    FreeFormFin.cp : tuple
+        Tuple with the x, y and z local coordinates of the fin set center of
+        pressure. Has units of length and is given in meters.
+    FreeFormFin.cpx : float
+        Fin set local center of pressure x coordinate. Has units of length and
+        is given in meters.
+    FreeFormFin.cpy : float
+        Fin set local center of pressure y coordinate. Has units of length and
+        is given in meters.
+    FreeFormFin.cpz : float
+        Fin set local center of pressure z coordinate. Has units of length and
+        is given in meters.
+    FreeFormFin.cl : Function
+        Function which defines the lift coefficient as a function of the angle
+        of attack and the Mach number. Takes as input the angle of attack in
+        radians and the Mach number. Returns the lift coefficient.
+    FreeFormFin.clalpha : float
+        Lift coefficient slope. Has units of 1/rad.
+    FreeFormFin.mac_length : float
+        Mean aerodynamic chord length of the fin set.
+    FreeFormFin.mac_lead : float
+        Mean aerodynamic chord leading edge x coordinate.
+    """
+
+    def __init__(
+        self,
+        angular_position,
+        shape_points,
+        rocket_radius,
+        cant_angle=0,
+        airfoil=None,
+        name="Free Form Fin",
+    ):
+        """Initialize FreeFormFin class.
+
+        Parameters
+        ----------
+        angular_position : float
+            Angular position of the fin in degrees measured as the rotation
+            around the symmetry axis of the rocket relative to one of the other
+            principal axis. See :ref:`Angular Position Inputs <angular_position>`
+        shape_points : list
+            List of tuples (x, y) containing the coordinates of the fin's
+            geometry defining points. The point (0, 0) is the root leading edge.
+            Positive x is rearwards, positive y is upwards (span direction).
+            The shape will be interpolated between the points, in the order
+            they are given. The last point connects to the first point, and
+            represents the trailing edge.
+        rocket_radius : int, float
+            Reference radius to calculate lift coefficient, in meters.
+        cant_angle : int, float, optional
+            Fins cant angle with respect to the rocket centerline. Must
+            be given in degrees.
+        airfoil : tuple, optional
+            Default is null, in which case fins will be treated as flat plates.
+            Otherwise, if tuple, fins will be considered as airfoils. The
+            tuple's first item specifies the airfoil's lift coefficient
+            by angle of attack and must be either a .csv, .txt, ndarray
+            or callable. The .csv and .txt files can contain a single line
+            header and the first column must specify the angle of attack, while
+            the second column must specify the lift coefficient. The
+            ndarray should be as [(x0, y0), (x1, y1), (x2, y2), ...]
+            where x0 is the angle of attack and y0 is the lift coefficient.
+            If callable, it should take an angle of attack as input and
+            return the lift coefficient at that angle of attack.
+            The tuple's second item is the unit of the angle of attack,
+            accepting either "radians" or "degrees".
+        name : str
+            Name of the free form fin.
+
+        Returns
+        -------
+        None
+        """
+        root_chord, span = _FreeFormGeometry.infer_dimensions(shape_points)
+
+        super().__init__(
+            angular_position,
+            root_chord,
+            span,
+            rocket_radius,
+            cant_angle,
+            airfoil,
+            name,
+        )
+
+        self.geometry = _FreeFormGeometry(self, shape_points)
+        self._update_geometry_chain()
+        self.evaluate_shape()
+        self.evaluate_rotation_matrix()
+
+        self.prints = _FreeFormFinPrints(self)
+        self.plots = _FreeFormFinPlots(self)
+
+    def evaluate_center_of_pressure(self):
+        """Calculates and returns the center of pressure of the fin in local
+        coordinates. The center of pressure position is saved and stored as a
+        tuple.
+
+        Returns
+        -------
+        None
+        """
+        # Center of pressure position in local coordinates
+        cpz = self.mac_lead + 0.25 * self.mac_length
+        self.cpx = 0
+        self.cpy = self.Yma
+        self.cpz = cpz
+        self.cp = (self.cpx, self.cpy, self.cpz)
+
+    @property
+    def shape_points(self):
+        return self.geometry.shape_points
+
+    def to_dict(self, **kwargs):
+        data = super().to_dict(**kwargs)
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
+        return data
+
+    @classmethod
+    def from_dict(cls, data):
+        return cls(
+            angular_position=data["angular_position"],
+            shape_points=data["shape_points"],
+            rocket_radius=data["rocket_radius"],
+            cant_angle=data["cant_angle"],
+            airfoil=data["airfoil"],
+            name=data["name"],
+        )
diff --git a/rocketpy/rocket/aero_surface/fins/free_form_fins.py b/rocketpy/rocket/aero_surface/fins/free_form_fins.py
index 72758171e..d7c7e9512 100644
--- a/rocketpy/rocket/aero_surface/fins/free_form_fins.py
+++ b/rocketpy/rocket/aero_surface/fins/free_form_fins.py
@@ -1,9 +1,6 @@
-import warnings
-
-import numpy as np
-
 from rocketpy.plots.aero_surface_plots import _FreeFormFinsPlots
 from rocketpy.prints.aero_surface_prints import _FreeFormFinsPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _FreeFormGeometry
 
 from .fins import Fins
 
@@ -45,9 +42,9 @@ class FreeFormFins(Fins):
         Fin span in meters.
     FreeFormFins.name : string
         Name of fin set.
-    FreeFormFins.d : float
+    FreeFormFins.rocket_diameter : float
         Reference diameter of the rocket, in meters.
-    FreeFormFins.ref_area : float
+    FreeFormFins.reference_area : float
         Reference area of the rocket, in m².
     FreeFormFins.Af : float
         Area of the longitudinal section of each fin in the set.
@@ -135,23 +132,7 @@ def __init__(
         -------
         None
         """
-        self.shape_points = shape_points
-
-        down = False
-        for i in range(1, len(shape_points)):
-            if shape_points[i][1] > shape_points[i - 1][1] and down:
-                warnings.warn(
-                    "Jagged fin shape detected. This may cause small inaccuracies "
-                    "center of pressure and pitch moment calculations."
-                )
-                break
-            if shape_points[i][1] < shape_points[i - 1][1]:
-                down = True
-            i += 1
-
-        root_chord = abs(shape_points[0][0] - shape_points[-1][0])
-        ys = [point[1] for point in shape_points]
-        span = max(ys) - min(ys)
+        root_chord, span = _FreeFormGeometry.infer_dimensions(shape_points)
 
         super().__init__(
             n,
@@ -163,10 +144,9 @@ def __init__(
             name,
         )
 
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry = _FreeFormGeometry(self, shape_points)
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
         self.prints = _FreeFormFinsPrints(self)
         self.plots = _FreeFormFinsPlots(self)
@@ -187,215 +167,24 @@ def evaluate_center_of_pressure(self):
         self.cpz = cpz
         self.cp = (self.cpx, self.cpy, self.cpz)
 
-    def evaluate_geometrical_parameters(self):  # pylint: disable=too-many-statements
-        """
-        Calculates and saves the fin set's geometrical parameters such as the
-        fin area, aspect ratio, and parameters related to roll movement. This
-        method uses the same calculations to those in OpenRocket for free-form
-        fin shapes.
-
-        Returns
-        -------
-        None
-        """
-        # pylint: disable=invalid-name
-        # pylint: disable=too-many-locals
-        # Calculate the fin area (Af) using the Shoelace theorem (polygon area formula)
-        Af = 0
-        for i in range(len(self.shape_points) - 1):
-            x1, y1 = self.shape_points[i]
-            x2, y2 = self.shape_points[i + 1]
-            Af += (y1 + y2) * (x1 - x2)
-        Af = abs(Af) / 2
-        if Af < 1e-6:
-            raise ValueError("Fin area is too small. Check the shape_points.")
-
-        # Calculate aspect ratio (AR) and lift interference factors
-        AR = 2 * self.span**2 / Af  # Aspect ratio
-        tau = (self.span + self.rocket_radius) / self.rocket_radius
-        lift_interference_factor = 1 + 1 / tau
-
-        # Calculate roll forcing interference factor using OpenRocket's approach
-        roll_forcing_interference_factor = (1 / np.pi**2) * (
-            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
-            + ((np.pi * (tau**2 + 1) ** 2) / (tau**2 * (tau - 1) ** 2))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
-            + ((tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
-            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
-            - (4 * (tau + 1))
-            / (tau * (tau - 1))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
-        )
-
-        # Define number of interpolation points along the span of the fin
-        points_per_line = 40  # Same as OpenRocket
-
-        # Initialize arrays for leading/trailing edge and chord lengths
-        chord_lead = np.ones(points_per_line) * np.inf  # Leading edge x coordinates
-        chord_trail = np.ones(points_per_line) * -np.inf  # Trailing edge x coordinates
-        chord_length = np.zeros(
-            points_per_line
-        )  # Chord length for each spanwise section
-
-        # Discretize fin shape and calculate chord length, leading, and trailing edges
-        for p in range(1, len(self.shape_points)):
-            x1, y1 = self.shape_points[p - 1]
-            x2, y2 = self.shape_points[p]
-
-            # Compute corresponding points along the fin span (clamp to valid range)
-            prev_idx = int(y1 / self.span * (points_per_line - 1))
-            curr_idx = int(y2 / self.span * (points_per_line - 1))
-            prev_idx = np.clip(prev_idx, 0, points_per_line - 1)
-            curr_idx = np.clip(curr_idx, 0, points_per_line - 1)
-
-            if prev_idx > curr_idx:
-                prev_idx, curr_idx = curr_idx, prev_idx
-
-            # Compute intersection of fin edge with each spanwise section
-            for i in range(prev_idx, curr_idx + 1):
-                y = i * self.span / (points_per_line - 1)
-                if y1 != y2:
-                    x = np.clip(
-                        (y - y2) / (y1 - y2) * x1 + (y1 - y) / (y1 - y2) * x2,
-                        min(x1, x2),
-                        max(x1, x2),
-                    )
-                else:
-                    x = x1  # Handle horizontal segments
-
-                # Update leading and trailing edge positions
-                chord_lead[i] = min(chord_lead[i], x)
-                chord_trail[i] = max(chord_trail[i], x)
-
-                # Update chord length
-                if y1 < y2:
-                    chord_length[i] -= x
-                else:
-                    chord_length[i] += x
-
-        # Replace infinities and handle invalid values in chord_lead and chord_trail
-        for i in range(points_per_line):
-            if (
-                np.isinf(chord_lead[i])
-                or np.isinf(chord_trail[i])
-                or np.isnan(chord_lead[i])
-                or np.isnan(chord_trail[i])
-            ):
-                chord_lead[i] = 0
-                chord_trail[i] = 0
-            if chord_length[i] < 0 or np.isnan(chord_length[i]):
-                chord_length[i] = 0
-            if chord_length[i] > chord_trail[i] - chord_lead[i]:
-                chord_length[i] = chord_trail[i] - chord_lead[i]
-
-        # Initialize integration variables for various aerodynamic and roll properties
-        radius = self.rocket_radius
-        total_area = 0
-        mac_length = 0  # Mean aerodynamic chord length
-        mac_lead = 0  # Mean aerodynamic chord leading edge
-        mac_span = 0  # Mean aerodynamic chord spanwise position (Yma)
-        cos_gamma_sum = 0  # Sum of cosine of the sweep angle
-        roll_geometrical_constant = 0
-        roll_damping_numerator = 0
-        roll_damping_denominator = 0
-
-        # Perform integration over spanwise sections
-        dy = self.span / (points_per_line - 1)
-        for i in range(points_per_line):
-            chord = chord_trail[i] - chord_lead[i]
-            y = i * dy
-
-            # Update integration variables
-            mac_length += chord * chord
-            mac_span += y * chord
-            mac_lead += chord_lead[i] * chord
-            total_area += chord
-            roll_geometrical_constant += chord_length[i] * (radius + y) ** 2
-            roll_damping_numerator += radius**3 * chord / (radius + y) ** 2
-            roll_damping_denominator += (radius + y) * chord
-
-            # Update cosine of sweep angle (cos_gamma)
-            if i > 0:
-                dx = (chord_trail[i] + chord_lead[i]) / 2 - (
-                    chord_trail[i - 1] + chord_lead[i - 1]
-                ) / 2
-                cos_gamma_sum += dy / np.hypot(dx, dy)
-
-        # Finalize mean aerodynamic chord properties
-        mac_length *= dy
-        mac_span *= dy
-        mac_lead *= dy
-        total_area *= dy
-        roll_geometrical_constant *= dy
-        roll_damping_numerator *= dy
-        roll_damping_denominator *= dy
-
-        mac_length /= total_area
-        mac_span /= total_area
-        mac_lead /= total_area
-        cos_gamma = cos_gamma_sum / (points_per_line - 1)
-
-        # Store computed values
-        self.Af = Af  # Fin area
-        self.AR = AR  # Aspect ratio
-        self.gamma_c = np.arccos(cos_gamma)  # Sweep angle
-        self.Yma = mac_span  # Mean aerodynamic chord spanwise position
-        self.mac_length = mac_length
-        self.mac_lead = mac_lead
-        self.tau = tau
-        self.roll_geometrical_constant = roll_geometrical_constant
-        self.lift_interference_factor = lift_interference_factor
-        self.roll_forcing_interference_factor = roll_forcing_interference_factor
-        self.roll_damping_interference_factor = 1 + (
-            roll_damping_numerator / roll_damping_denominator
-        )
-
-        # Evaluate the shape and finalize geometry
-        self.evaluate_shape()
-
-    def evaluate_shape(self):
-        x_array, y_array = zip(*self.shape_points)
-        self.shape_vec = [np.array(x_array), np.array(y_array)]
+    @property
+    def shape_points(self):
+        return self.geometry.shape_points
 
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
-        data["shape_points"] = self.shape_points
-
-        if kwargs.get("include_outputs", False):
-            data.update(
-                {
-                    "Af": self.Af,
-                    "AR": self.AR,
-                    "gamma_c": self.gamma_c,
-                    "Yma": self.Yma,
-                    "mac_length": self.mac_length,
-                    "mac_lead": self.mac_lead,
-                    "roll_geometrical_constant": self.roll_geometrical_constant,
-                    "tau": self.tau,
-                    "lift_interference_factor": self.lift_interference_factor,
-                    "roll_forcing_interference_factor": self.roll_forcing_interference_factor,
-                    "roll_damping_interference_factor": self.roll_damping_interference_factor,
-                }
-            )
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
         return data
 
     @classmethod
     def from_dict(cls, data):
         return cls(
-            data["n"],
-            data["shape_points"],
-            data["rocket_radius"],
-            data["cant_angle"],
-            data["airfoil"],
-            data["name"],
+            n=data["n"],
+            shape_points=data["shape_points"],
+            rocket_radius=data["rocket_radius"],
+            cant_angle=data["cant_angle"],
+            airfoil=data["airfoil"],
+            name=data["name"],
         )
-
-    def info(self):
-        self.prints.geometry()
-        self.prints.lift()
-
-    def all_info(self):
-        self.prints.all()
-        self.plots.all()
diff --git a/rocketpy/rocket/aero_surface/fins/trapezoidal_fin.py b/rocketpy/rocket/aero_surface/fins/trapezoidal_fin.py
new file mode 100644
index 000000000..872aebe97
--- /dev/null
+++ b/rocketpy/rocket/aero_surface/fins/trapezoidal_fin.py
@@ -0,0 +1,242 @@
+from rocketpy.plots.aero_surface_plots import _TrapezoidalFinPlots
+from rocketpy.prints.aero_surface_prints import _TrapezoidalFinPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _TrapezoidalGeometry
+
+from .fin import Fin
+
+
+class TrapezoidalFin(Fin):
+    """A class used to represent a single trapezoidal fin.
+
+    This class inherits from the Fin class.
+
+    Note
+    ----
+    Local coordinate system:
+        - Origin located at the top of the root chord.
+        - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+        - Y axis perpendicular to the Z axis, in the span direction, positive upwards.
+        - X axis completes the right-handed coordinate system.
+
+    See Also
+    --------
+    Fin : Parent class
+
+    Attributes
+    ----------
+    TrapezoidalFin.angular_position : float
+        Angular position of the fin set with respect to the rocket centerline,
+        in degrees.
+    TrapezoidalFin.rocket_radius : float
+        The reference rocket radius used for lift coefficient normalization, in
+        meters.
+    TrapezoidalFin.airfoil : tuple
+        Tuple of two items. First is the airfoil lift curve.
+        Second is the unit of the curve (radians or degrees).
+    TrapezoidalFin.cant_angle : float
+        Fins cant angle with respect to the rocket centerline, in degrees.
+    TrapezoidalFin.cant_angle_rad : float
+        Fins cant angle with respect to the rocket centerline, in radians.
+    TrapezoidalFin.root_chord : float
+        Fin root chord in meters.
+    TrapezoidalFin.tip_chord : float
+        Fin tip chord in meters.
+    TrapezoidalFin.span : float
+        Fin span in meters.
+    TrapezoidalFin.name : string
+        Name of fin set.
+    TrapezoidalFin.sweep_length : float
+        Fins sweep length in meters. By sweep length, understand the axial
+        distance between the fin root leading edge and the fin tip leading edge
+        measured parallel to the rocket centerline.
+    TrapezoidalFin.sweep_angle : float
+        Fins sweep angle with respect to the rocket centerline. Must
+        be given in degrees.
+    TrapezoidalFin.rocket_diameter : float
+        Reference diameter of the rocket, in meters.
+    TrapezoidalFins.fin_area : float
+        Area of the longitudinal section of each fin in the set.
+    TrapezoidalFins.AR : float
+        Aspect ratio of the fin.
+    TrapezoidalFin.gamma_c : float
+        Fin mid-chord sweep angle.
+    TrapezoidalFin.yma : float
+        Span wise position of the mean aerodynamic chord.
+    TrapezoidalFin.roll_geometrical_constant : float
+        Geometrical constant used in roll calculations.
+    TrapezoidalFin.tau : float
+        Geometrical relation used to simplify lift and roll calculations.
+    TrapezoidalFin.lift_interference_factor : float
+        Factor of Fin-Body interference in the lift coefficient.
+    TrapezoidalFin.cp : tuple
+        Tuple with the x, y and z local coordinates of the fin set center of
+        pressure. Has units of length and is given in meters.
+    TrapezoidalFin.cpx : float
+        Fin set local center of pressure x coordinate. Has units of length and
+        is given in meters.
+    TrapezoidalFin.cpy : float
+        Fin set local center of pressure y coordinate. Has units of length and
+        is given in meters.
+    TrapezoidalFin.cpz : float
+        Fin set local center of pressure z coordinate. Has units of length and
+        is given in meters.
+    """
+
+    def __init__(
+        self,
+        angular_position,
+        root_chord,
+        tip_chord,
+        span,
+        rocket_radius,
+        cant_angle=0,
+        sweep_length=None,
+        sweep_angle=None,
+        airfoil=None,
+        name="Trapezoidal Fin",
+    ):
+        """Initializes the TrapezoidalFin class.
+
+        Parameters
+        ----------
+        angular_position : float
+            Angular position of the fin in degrees measured as the rotation
+            around the symmetry axis of the rocket relative to one of the other
+            principal axis. See :ref:`Angular Position Inputs <angular_position>`
+        root_chord : int, float
+            Fin root chord in meters.
+        tip_chord : int, float
+            Fin tip chord in meters.
+        span : int, float
+            Fin span in meters.
+        rocket_radius : int, float
+            Reference radius to calculate lift coefficient, in meters.
+        cant_angle : int, float, optional
+            Fins cant angle with respect to the rocket centerline. Must
+            be given in degrees.
+        sweep_length : int, float, optional
+            Fins sweep length in meters. By sweep length, understand the axial
+            distance between the fin root leading edge and the fin tip leading
+            edge measured parallel to the rocket centerline. If not given, the
+            sweep length is assumed to be equal the root chord minus the tip
+            chord, in which case the fin is a right trapezoid with its base
+            perpendicular to the rocket's axis. Cannot be used in conjunction
+            with sweep_angle.
+        sweep_angle : int, float, optional
+            Fins sweep angle with respect to the rocket centerline. Must
+            be given in degrees. If not given, the sweep angle is automatically
+            calculated, in which case the fin is assumed to be a right trapezoid
+            with its base perpendicular to the rocket's axis.
+            Cannot be used in conjunction with sweep_length.
+        airfoil : tuple, optional
+            Default is null, in which case fins will be treated as flat plates.
+            Otherwise, if tuple, fins will be considered as airfoils. The
+            tuple's first item specifies the airfoil's lift coefficient
+            by angle of attack and must be either a .csv, .txt, ndarray
+            or callable. The .csv and .txt files can contain a single line
+            header and the first column must specify the angle of attack, while
+            the second column must specify the lift coefficient. The
+            ndarray should be as [(x0, y0), (x1, y1), (x2, y2), ...]
+            where x0 is the angle of attack and y0 is the lift coefficient.
+            If callable, it should take an angle of attack as input and
+            return the lift coefficient at that angle of attack.
+            The tuple's second item is the unit of the angle of attack,
+            accepting either "radians" or "degrees".
+        name : str
+            Name of the trapezoidal fin.
+        """
+        super().__init__(
+            angular_position,
+            root_chord,
+            span,
+            rocket_radius,
+            cant_angle,
+            airfoil,
+            name,
+        )
+
+        self.geometry = _TrapezoidalGeometry(
+            self,
+            tip_chord=tip_chord,
+            sweep_length=sweep_length,
+            sweep_angle=sweep_angle,
+        )
+        self._update_geometry_chain()
+        self.evaluate_shape()
+        self.evaluate_rotation_matrix()
+
+        self.prints = _TrapezoidalFinPrints(self)
+        self.plots = _TrapezoidalFinPlots(self)
+
+    @property
+    def tip_chord(self):
+        return self.geometry.tip_chord
+
+    @tip_chord.setter
+    def tip_chord(self, value):
+        self.geometry.tip_chord = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
+
+    @property
+    def sweep_angle(self):
+        return self.geometry.sweep_angle
+
+    @sweep_angle.setter
+    def sweep_angle(self, value):
+        self.geometry.sweep_angle = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
+
+    @property
+    def sweep_length(self):
+        return self.geometry.sweep_length
+
+    @sweep_length.setter
+    def sweep_length(self, value):
+        self.geometry.sweep_length = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
+
+    def evaluate_center_of_pressure(self):
+        """Calculates and returns the center of pressure of the fin in local
+        coordinates. The center of pressure position is saved and stored as a
+        tuple.
+
+        Returns
+        -------
+        None
+        """
+        # Center of pressure position in local coordinates
+        cpz = (self.sweep_length / 3) * (
+            (self.root_chord + 2 * self.tip_chord) / (self.root_chord + self.tip_chord)
+        ) + (1 / 6) * (
+            self.root_chord
+            + self.tip_chord
+            - self.root_chord * self.tip_chord / (self.root_chord + self.tip_chord)
+        )
+        self.cpx = 0
+        self.cpy = self.Yma
+        self.cpz = cpz
+        self.cp = (self.cpx, self.cpy, self.cpz)
+
+    def to_dict(self, **kwargs):
+        data = super().to_dict(**kwargs)
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
+        return data
+
+    @classmethod
+    def from_dict(cls, data):
+        return cls(
+            angular_position=data["angular_position"],
+            root_chord=data["root_chord"],
+            tip_chord=data["tip_chord"],
+            span=data["span"],
+            rocket_radius=data["rocket_radius"],
+            cant_angle=data["cant_angle"],
+            sweep_length=data.get("sweep_length"),
+            airfoil=data["airfoil"],
+            name=data["name"],
+        )
diff --git a/rocketpy/rocket/aero_surface/fins/trapezoidal_fins.py b/rocketpy/rocket/aero_surface/fins/trapezoidal_fins.py
index c6b4ea633..2c9adea58 100644
--- a/rocketpy/rocket/aero_surface/fins/trapezoidal_fins.py
+++ b/rocketpy/rocket/aero_surface/fins/trapezoidal_fins.py
@@ -1,7 +1,6 @@
-import numpy as np
-
 from rocketpy.plots.aero_surface_plots import _TrapezoidalFinsPlots
 from rocketpy.prints.aero_surface_prints import _TrapezoidalFinsPrints
+from rocketpy.rocket.aero_surface.fins._geometry import _TrapezoidalGeometry
 
 from .fins import Fins
 
@@ -35,9 +34,6 @@ class TrapezoidalFins(Fins):
         Second is the unit of the curve (radians or degrees).
     TrapezoidalFins.cant_angle : float
         Fins cant angle with respect to the rocket centerline, in degrees.
-    TrapezoidalFins.changing_attribute_dict : dict
-        Dictionary that stores the name and the values of the attributes that
-        may be changed during a simulation. Useful for control systems.
     TrapezoidalFins.cant_angle_rad : float
         Fins cant angle with respect to the rocket centerline, in radians.
     TrapezoidalFins.root_chord : float
@@ -55,9 +51,9 @@ class TrapezoidalFins(Fins):
     TrapezoidalFins.sweep_angle : float
         Fins sweep angle with respect to the rocket centerline. Must
         be given in degrees.
-    TrapezoidalFins.d : float
+    TrapezoidalFins.rocket_diameter : float
         Reference diameter of the rocket, in meters.
-    TrapezoidalFins.ref_area : float
+    TrapezoidalFins.reference_area : float
         Reference area of the rocket, in m².
     TrapezoidalFins.Af : float
         Area of the longitudinal section of each fin in the set.
@@ -169,62 +165,47 @@ def __init__(
             name,
         )
 
-        # Check if sweep angle or sweep length is given
-        if sweep_length is not None and sweep_angle is not None:
-            raise ValueError("Cannot use sweep_length and sweep_angle together")
-        elif sweep_angle is not None:
-            sweep_length = np.tan(sweep_angle * np.pi / 180) * span
-        elif sweep_length is None:
-            sweep_length = root_chord - tip_chord
-
-        self._tip_chord = tip_chord
-        self._sweep_length = sweep_length
-        self._sweep_angle = sweep_angle
-
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry = _TrapezoidalGeometry(
+            self,
+            tip_chord=tip_chord,
+            sweep_length=sweep_length,
+            sweep_angle=sweep_angle,
+        )
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
         self.prints = _TrapezoidalFinsPrints(self)
         self.plots = _TrapezoidalFinsPlots(self)
 
     @property
     def tip_chord(self):
-        return self._tip_chord
+        return self.geometry.tip_chord
 
     @tip_chord.setter
     def tip_chord(self, value):
-        self._tip_chord = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry.tip_chord = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
     @property
     def sweep_angle(self):
-        return self._sweep_angle
+        return self.geometry.sweep_angle
 
     @sweep_angle.setter
     def sweep_angle(self, value):
-        self._sweep_angle = value
-        self._sweep_length = np.tan(value * np.pi / 180) * self.span
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry.sweep_angle = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
     @property
     def sweep_length(self):
-        return self._sweep_length
+        return self.geometry.sweep_length
 
     @sweep_length.setter
     def sweep_length(self, value):
-        self._sweep_length = value
-        self.evaluate_geometrical_parameters()
-        self.evaluate_center_of_pressure()
-        self.evaluate_lift_coefficient()
-        self.evaluate_roll_parameters()
+        self.geometry.sweep_length = value
+        self._update_geometry_chain()
+        self.evaluate_shape()
 
     def evaluate_center_of_pressure(self):
         """Calculates and returns the center of pressure of the fin set in local
@@ -248,124 +229,11 @@ def evaluate_center_of_pressure(self):
         self.cpz = cpz
         self.cp = (self.cpx, self.cpy, self.cpz)
 
-    def evaluate_geometrical_parameters(self):  # pylint: disable=too-many-statements
-        """Calculates and saves fin set's geometrical parameters such as the
-        fins' area, aspect ratio and parameters for roll movement.
-
-        Returns
-        -------
-        None
-        """
-        # pylint: disable=invalid-name
-        Yr = self.root_chord + self.tip_chord
-        Af = Yr * self.span / 2  # Fin area
-        AR = 2 * self.span**2 / Af  # Fin aspect ratio
-        gamma_c = np.arctan(
-            (self.sweep_length + 0.5 * self.tip_chord - 0.5 * self.root_chord)
-            / (self.span)
-        )
-        Yma = (
-            (self.span / 3) * (self.root_chord + 2 * self.tip_chord) / Yr
-        )  # Span wise coord of mean aero chord
-
-        # Fin–body interference correction parameters
-        tau = (self.span + self.rocket_radius) / self.rocket_radius
-        lift_interference_factor = 1 + 1 / tau
-        lambda_ = self.tip_chord / self.root_chord
-
-        # Parameters for Roll Moment.
-        # Documented at: https://docs.rocketpy.org/en/latest/technical/
-        roll_geometrical_constant = (
-            (self.root_chord + 3 * self.tip_chord) * self.span**3
-            + 4
-            * (self.root_chord + 2 * self.tip_chord)
-            * self.rocket_radius
-            * self.span**2
-            + 6 * (self.root_chord + self.tip_chord) * self.span * self.rocket_radius**2
-        ) / 12
-        roll_damping_interference_factor = 1 + (
-            ((tau - lambda_) / (tau)) - ((1 - lambda_) / (tau - 1)) * np.log(tau)
-        ) / (
-            ((tau + 1) * (tau - lambda_)) / (2)
-            - ((1 - lambda_) * (tau**3 - 1)) / (3 * (tau - 1))
-        )
-        roll_forcing_interference_factor = (1 / np.pi**2) * (
-            (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
-            + ((np.pi * (tau**2 + 1) ** 2) / (tau**2 * (tau - 1) ** 2))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
-            + ((tau**2 + 1) ** 2)
-            / (tau**2 * (tau - 1) ** 2)
-            * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
-            - (4 * (tau + 1))
-            / (tau * (tau - 1))
-            * np.arcsin((tau**2 - 1) / (tau**2 + 1))
-            + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
-        )
-
-        # Store values
-        self.Yr = Yr
-        self.Af = Af  # Fin area
-        self.AR = AR  # Aspect Ratio
-        self.gamma_c = gamma_c  # Mid chord angle
-        self.Yma = Yma  # Span wise coord of mean aero chord
-        self.roll_geometrical_constant = roll_geometrical_constant
-        self.tau = tau
-        self.lift_interference_factor = lift_interference_factor
-        self.λ = lambda_  # pylint: disable=non-ascii-name
-        self.roll_damping_interference_factor = roll_damping_interference_factor
-        self.roll_forcing_interference_factor = roll_forcing_interference_factor
-
-        self.evaluate_shape()
-
-    def evaluate_shape(self):
-        if self.sweep_length:
-            points = [
-                (0, 0),
-                (self.sweep_length, self.span),
-                (self.sweep_length + self.tip_chord, self.span),
-                (self.root_chord, 0),
-            ]
-        else:
-            points = [
-                (0, 0),
-                (self.root_chord - self.tip_chord, self.span),
-                (self.root_chord, self.span),
-                (self.root_chord, 0),
-            ]
-
-        x_array, y_array = zip(*points)
-        self.shape_vec = [np.array(x_array), np.array(y_array)]
-
-    def info(self):
-        self.prints.geometry()
-        self.prints.lift()
-
-    def all_info(self):
-        self.prints.all()
-        self.plots.all()
-
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
-        data["tip_chord"] = self.tip_chord
-        data["sweep_length"] = self.sweep_length
-        data["sweep_angle"] = self.sweep_angle
-
-        if kwargs.get("include_outputs", False):
-            data.update(
-                {
-                    "shape_vec": self.shape_vec,
-                    "Af": self.Af,
-                    "AR": self.AR,
-                    "gamma_c": self.gamma_c,
-                    "Yma": self.Yma,
-                    "roll_geometrical_constant": self.roll_geometrical_constant,
-                    "tau": self.tau,
-                    "lift_interference_factor": self.lift_interference_factor,
-                    "roll_damping_interference_factor": self.roll_damping_interference_factor,
-                    "roll_forcing_interference_factor": self.roll_forcing_interference_factor,
-                }
-            )
+        data.update(
+            self.geometry.get_data(include_outputs=kwargs.get("include_outputs", False))
+        )
         return data
 
     @classmethod
diff --git a/rocketpy/rocket/aero_surface/generic_surface.py b/rocketpy/rocket/aero_surface/generic_surface.py
index 8ab438620..d1ae3a8f0 100644
--- a/rocketpy/rocket/aero_surface/generic_surface.py
+++ b/rocketpy/rocket/aero_surface/generic_surface.py
@@ -85,6 +85,8 @@ def __init__(
         self.cpz = center_of_pressure[2]
         self.name = name
 
+        self._rotation_surface_to_body = Matrix([[1, 0, 0], [0, 1, 0], [0, 0, 1]])
+
         default_coefficients = self._get_default_coefficients()
         self._check_coefficients(coefficients, default_coefficients)
         coefficients = self._complete_coefficients(coefficients, default_coefficients)
diff --git a/rocketpy/rocket/aero_surface/nose_cone.py b/rocketpy/rocket/aero_surface/nose_cone.py
index 240a61a5c..fb2ac85d2 100644
--- a/rocketpy/rocket/aero_surface/nose_cone.py
+++ b/rocketpy/rocket/aero_surface/nose_cone.py
@@ -1,3 +1,4 @@
+import logging
 import warnings
 
 import numpy as np
@@ -9,6 +10,8 @@
 
 from .aero_surface import AeroSurface
 
+logger = logging.getLogger(__name__)
+
 
 class NoseCone(AeroSurface):
     """Keeps nose cone information.
@@ -445,9 +448,11 @@ def final_shape(x):
         self.shape_vec = [nosecone_x, nosecone_y]
         if abs(nosecone_x[-1] - self.length) >= 0.001:  # 1 millimeter
             self._length = nosecone_x[-1]
-            print(
-                "Due to the chosen bluffness ratio, the nose "
-                f"cone length was reduced to {self.length} m."
+            warnings.warn(
+                f"Due to the chosen bluffness ratio, the nose cone length was "
+                f"reduced to {self.length:.4f} m.",
+                UserWarning,
+                stacklevel=2,
             )
         self.fineness_ratio = self.length / (2 * self.base_radius)
 
diff --git a/rocketpy/rocket/aero_surface/rail_buttons.py b/rocketpy/rocket/aero_surface/rail_buttons.py
index 89331c99f..7d3a9bd30 100644
--- a/rocketpy/rocket/aero_surface/rail_buttons.py
+++ b/rocketpy/rocket/aero_surface/rail_buttons.py
@@ -17,6 +17,7 @@ class RailButtons(AeroSurface):
         Angular position of the rail buttons in degrees measured
         as the rotation around the symmetry axis of the rocket
         relative to one of the other principal axis.
+        See :ref:`Angular Position Inputs <angular_position>`
     RailButtons.angular_position_rad : float
         Angular position of the rail buttons in radians.
     RailButtons.button_height : float, optional
diff --git a/rocketpy/rocket/components.py b/rocketpy/rocket/components.py
index 9ce8595b3..57e4d12f8 100644
--- a/rocketpy/rocket/components.py
+++ b/rocketpy/rocket/components.py
@@ -1,4 +1,5 @@
 from collections import namedtuple
+from copy import deepcopy
 
 
 class Components:
@@ -186,7 +187,7 @@ def clear(self):
         self._components.clear()
 
     def sort_by_position(self, reverse=False):
-        """Sort the list of components by z axis position.
+        """Returns a new Components object sorted components by z axis position.
 
         Parameters
         ----------
@@ -196,9 +197,12 @@ def sort_by_position(self, reverse=False):
 
         Returns
         -------
-        None
+        Components
+            A new Components object sorted by component position.
         """
-        self._components.sort(key=lambda x: x.position.z, reverse=reverse)
+        components = deepcopy(self)
+        components._components.sort(key=lambda x: x.position.z, reverse=reverse)
+        return components
 
     def to_dict(self, **kwargs):  # pylint: disable=unused-argument
         return {
diff --git a/rocketpy/rocket/parachute.py b/rocketpy/rocket/parachute.py
index 4e0318d18..137e98e3a 100644
--- a/rocketpy/rocket/parachute.py
+++ b/rocketpy/rocket/parachute.py
@@ -1,408 +1,23 @@
-from inspect import signature
+"""Backward-compatibility shim for the relocated parachute module.
 
-import numpy as np
+The parachute classes moved from ``rocketpy.rocket.parachute`` to the
+``rocketpy.rocket.parachutes`` subpackage, and the old concrete ``Parachute``
+class became an abstract base with the hemispherical model split out into
+``HemisphericalParachute``. Importing from this module still works for backward
+compatibility but is deprecated and will be removed in v1.15.0.
+"""
 
-from rocketpy.tools import from_hex_decode, to_hex_encode
+import warnings
 
-from ..mathutils.function import Function
-from ..prints.parachute_prints import _ParachutePrints
+from .parachutes.hemispherical_parachute import HemisphericalParachute
+from .parachutes.parachute import Parachute
 
+warnings.warn(
+    "Importing from 'rocketpy.rocket.parachute' is deprecated and will be "
+    "removed in v1.15.0. Import from 'rocketpy.rocket.parachutes' instead, "
+    "e.g. 'from rocketpy.rocket.parachutes import HemisphericalParachute'.",
+    DeprecationWarning,
+    stacklevel=2,
+)
 
-class Parachute:
-    """Keeps information of the parachute, which is modeled as a hemispheroid.
-
-    Attributes
-    ----------
-    Parachute.name : string
-        Parachute name, such as drogue and main. Has no impact in
-        simulation, as it is only used to display data in a more
-        organized matter.
-    Parachute.cd_s : float
-        Drag coefficient times reference area for parachute. It has units of
-        area and must be given in squared meters.
-    Parachute.trigger : callable, float, str
-        This parameter defines the trigger condition for the parachute ejection
-        system. It can be one of the following:
-
-        - A callable function that takes three arguments:
-          1. Freestream pressure in pascals.
-          2. Height in meters above ground level.
-          3. The state vector of the simulation, which is defined as:
-
-             `[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]`.
-
-          4. A list of sensors that are attached to the rocket. The most recent
-             measurements of the sensors are provided with the
-             ``sensor.measurement`` attribute. The sensors are listed in the same
-             order as they are added to the rocket.
-
-          The function should return ``True`` if the parachute ejection system
-          should be triggered and False otherwise. The function will be called
-          according to the specified sampling rate.
-
-        - A float value, representing an absolute height in meters. In this
-          case, the parachute will be ejected when the rocket reaches this height
-          above ground level.
-
-        - The string "apogee" which triggers the parachute at apogee, i.e.,
-          when the rocket reaches its highest point and starts descending.
-
-
-    Parachute.triggerfunc : function
-        Trigger function created from the trigger used to evaluate the trigger
-        condition for the parachute ejection system. It is a callable function
-        that takes three arguments: Freestream pressure in Pa, Height above
-        ground level in meters, and the state vector of the simulation. The
-        returns ``True`` if the parachute ejection system should be triggered
-        and ``False`` otherwise.
-
-        .. note:
-
-            The function will be called according to the sampling rate specified.
-
-    Parachute.sampling_rate : float
-        Sampling rate, in Hz, for the trigger function.
-    Parachute.lag : float
-        Time, in seconds, between the parachute ejection system is triggered
-        and the parachute is fully opened.
-    Parachute.noise : tuple, list
-        List in the format (mean, standard deviation, time-correlation).
-        The values are used to add noise to the pressure signal which is passed
-        to the trigger function. Default value is (0, 0, 0). Units are in Pa.
-    Parachute.noise_bias : float
-        Mean value of the noise added to the pressure signal, which is
-        passed to the trigger function. Unit is in Pa.
-    Parachute.noise_deviation : float
-        Standard deviation of the noise added to the pressure signal,
-        which is passed to the trigger function. Unit is in Pa.
-    Parachute.noise_corr : tuple, list
-        Tuple with the correlation between noise and time.
-    Parachute.noise_signal : list of tuple
-        List of (t, noise signal) corresponding to signal passed to
-        trigger function. Completed after running a simulation.
-    Parachute.noisy_pressure_signal : list of tuple
-        List of (t, noisy pressure signal) that is passed to the
-        trigger function. Completed after running a simulation.
-    Parachute.clean_pressure_signal : list of tuple
-        List of (t, clean pressure signal) corresponding to signal passed to
-        trigger function. Completed after running a simulation.
-    Parachute.noise_signal_function : Function
-        Function of noiseSignal.
-    Parachute.noisy_pressure_signal_function : Function
-        Function of noisy_pressure_signal.
-    Parachute.clean_pressure_signal_function : Function
-        Function of clean_pressure_signal.
-    Parachute.drag_coefficient : float
-        Drag coefficient of the inflated canopy shape, used only when
-        ``radius`` is not provided to estimate the parachute radius from
-        ``cd_s``: ``R = sqrt(cd_s / (drag_coefficient * pi))``. Typical
-        values: 1.4 for hemispherical canopies (default), 0.75 for flat
-        circular canopies, 1.5 for extended-skirt canopies.
-    Parachute.radius : float
-        Length of the non-unique semi-axis (radius) of the inflated hemispheroid
-        parachute in meters. If not provided at construction time, it is
-        estimated from ``cd_s`` and ``drag_coefficient``.
-    Parachute.height : float
-        Length of the unique semi-axis (height) of the inflated hemispheroid
-        parachute in meters.
-    Parachute.porosity : float
-        Geometric porosity of the canopy (ratio of open area to total canopy
-        area), in [0, 1]. Affects only the added-mass scaling during descent;
-        it does not change ``cd_s`` (drag). The default value of 0.0432 is
-        chosen so that the resulting ``added_mass_coefficient`` equals
-        approximately 1.0 ("neutral" added-mass behavior).
-    Parachute.added_mass_coefficient : float
-        Coefficient used to calculate the added-mass due to dragged air. It is
-        calculated from the porosity of the parachute.
-    """
-
-    def __init__(
-        self,
-        name,
-        cd_s,
-        trigger,
-        sampling_rate,
-        lag=0,
-        noise=(0, 0, 0),
-        radius=None,
-        height=None,
-        porosity=0.0432,
-        drag_coefficient=1.4,
-    ):
-        """Initializes Parachute class.
-
-        Parameters
-        ----------
-        name : string
-            Parachute name, such as drogue and main. Has no impact in
-            simulation, as it is only used to display data in a more
-            organized matter.
-        cd_s : float
-            Drag coefficient times reference area of the parachute.
-        trigger : callable, float, str
-            Defines the trigger condition for the parachute ejection system. It
-            can be one of the following:
-
-            - A callable function that takes three arguments: \
-
-                1. Freestream pressure in pascals.
-                2. Height in meters above ground level.
-                3. The state vector of the simulation, which is defined as: \
-
-                    .. code-block:: python
-
-                        u = [x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]
-
-                .. note::
-
-                    The function should return ``True`` if the parachute \
-                    ejection system should be triggered and ``False`` otherwise.
-            - A float value, representing an absolute height in meters. In this \
-                case, the parachute will be ejected when the rocket reaches this \
-                height above ground level.
-            - The string "apogee" which triggers the parachute at apogee, i.e., \
-                when the rocket reaches its highest point and starts descending.
-
-            .. note::
-
-                The function will be called according to the sampling rate specified.
-        sampling_rate : float
-            Sampling rate in which the parachute trigger will be checked at.
-            It is used to simulate the refresh rate of onboard sensors such
-            as barometers. Default value is 100. Value must be given in hertz.
-        lag : float, optional
-            Time between the parachute ejection system is triggered and the
-            parachute is fully opened. During this time, the simulation will
-            consider the rocket as flying without a parachute. Default value
-            is 0. Must be given in seconds.
-        noise : tuple, list, optional
-            List in the format (mean, standard deviation, time-correlation).
-            The values are used to add noise to the pressure signal which is
-            passed to the trigger function. Default value is ``(0, 0, 0)``.
-            Units are in Pa.
-        radius : float, optional
-            Length of the non-unique semi-axis (radius) of the inflated
-            hemispheroid parachute. If not provided, it is estimated from
-            ``cd_s`` and ``drag_coefficient`` using:
-            ``radius = sqrt(cd_s / (drag_coefficient * pi))``.
-            Units are in meters.
-        height : float, optional
-            Length of the unique semi-axis (height) of the inflated hemispheroid
-            parachute. Default value is the radius of the parachute.
-            Units are in meters.
-        porosity : float, optional
-            Geometric porosity of the canopy (ratio of open area to total
-            canopy area), in [0, 1]. Affects only the added-mass scaling
-            during descent; it does not change ``cd_s`` (drag). The default
-            value of 0.0432 is chosen so that the resulting
-            ``added_mass_coefficient`` equals approximately 1.0 ("neutral"
-            added-mass behavior).
-        drag_coefficient : float, optional
-            Drag coefficient of the inflated canopy shape, used only when
-            ``radius`` is not provided. It relates the aerodynamic ``cd_s``
-            to the physical canopy area via
-            ``cd_s = drag_coefficient * pi * radius**2``. Typical values:
-
-            - **1.4** — hemispherical canopy (default, NASA SP-8066)
-            - **0.75** — flat circular canopy
-            - **1.5** — extended-skirt canopy
-
-            Has no effect when ``radius`` is explicitly provided.
-        """
-
-        # Save arguments as attributes
-        self.name = name
-        self.cd_s = cd_s
-        self.trigger = trigger
-        self.sampling_rate = sampling_rate
-        self.lag = lag
-        self.noise = noise
-        self.drag_coefficient = drag_coefficient
-        self.porosity = porosity
-
-        # Initialize derived attributes
-        self.radius = self.__resolve_radius(radius, cd_s, drag_coefficient)
-        self.height = self.__resolve_height(height, self.radius)
-        self.added_mass_coefficient = self.__compute_added_mass_coefficient(
-            self.porosity
-        )
-        self.__init_noise(noise)
-        self.__evaluate_trigger_function(trigger)
-
-        # Prints and plots
-        self.prints = _ParachutePrints(self)
-
-    def __resolve_radius(self, radius, cd_s, drag_coefficient):
-        """Resolves parachute radius from input or aerodynamic relation."""
-        if radius is not None:
-            return radius
-
-        # cd_s = Cd * S = Cd * pi * R^2  =>  R = sqrt(cd_s / (Cd * pi))
-        return np.sqrt(cd_s / (drag_coefficient * np.pi))
-
-    def __resolve_height(self, height, radius):
-        """Resolves parachute height defaulting to radius when not provided."""
-        return height or radius
-
-    def __compute_added_mass_coefficient(self, porosity):
-        """Computes the added-mass coefficient from canopy porosity."""
-        return 1.068 * (
-            1 - 1.465 * porosity - 0.25975 * porosity**2 + 1.2626 * porosity**3
-        )
-
-    def __init_noise(self, noise):
-        """Initializes all noise-related attributes.
-
-        Parameters
-        ----------
-        noise : tuple, list
-            List in the format (mean, standard deviation, time-correlation).
-        """
-        self.noise_signal = [[-1e-6, np.random.normal(noise[0], noise[1])]]
-        self.noisy_pressure_signal = []
-        self.clean_pressure_signal = []
-        self.noise_bias = noise[0]
-        self.noise_deviation = noise[1]
-        self.noise_corr = (noise[2], (1 - noise[2] ** 2) ** 0.5)
-        self.clean_pressure_signal_function = Function(0)
-        self.noisy_pressure_signal_function = Function(0)
-        self.noise_signal_function = Function(0)
-        alpha, beta = self.noise_corr
-        self.noise_function = lambda: (
-            alpha * self.noise_signal[-1][1]
-            + beta * np.random.normal(noise[0], noise[1])
-        )
-
-    def __evaluate_trigger_function(self, trigger):
-        """This is used to set the triggerfunc attribute that will be used to
-        interact with the Flight class.
-        """
-        # pylint: disable=unused-argument, function-redefined
-
-        # Case 1: The parachute is deployed by a custom function
-        if callable(trigger):
-            # work around for having added sensors to parachute triggers
-            # to avoid breaking changes
-            triggerfunc = trigger
-            sig = signature(triggerfunc)
-            if len(sig.parameters) == 3:
-
-                def triggerfunc(p, h, y, sensors):
-                    return trigger(p, h, y)
-
-            self.triggerfunc = triggerfunc
-
-        # Case 2: The parachute is deployed at a given height
-        elif isinstance(trigger, (int, float)):
-            # The parachute is deployed at a given height
-            def triggerfunc(p, h, y, sensors):
-                # p = pressure considering parachute noise signal
-                # h = height above ground level considering parachute noise signal
-                # y = [x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]
-                return y[5] < 0 and h < trigger
-
-            self.triggerfunc = triggerfunc
-
-        # Case 3: The parachute is deployed at apogee
-        elif trigger.lower() == "apogee":
-            # The parachute is deployed at apogee
-            def triggerfunc(p, h, y, sensors):
-                # p = pressure considering parachute noise signal
-                # h = height above ground level considering parachute noise signal
-                # y = [x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]
-                return y[5] < 0
-
-            self.triggerfunc = triggerfunc
-
-        # Case 4: Invalid trigger input
-        else:
-            raise ValueError(
-                f"Unable to set the trigger function for parachute '{self.name}'. "
-                + "Trigger must be a callable, a float value or the string 'apogee'. "
-                + "See the Parachute class documentation for more information."
-            )
-
-    def __str__(self):
-        """Returns a string representation of the Parachute class.
-
-        Returns
-        -------
-        string
-            String representation of Parachute class. It is human readable.
-        """
-        return f"Parachute {self.name.title()} with a cd_s of {self.cd_s:.4f} m2"
-
-    def __repr__(self):
-        """Representation method for the class, useful when debugging."""
-        return (
-            f"<Parachute {self.name} "
-            + f"(cd_s = {self.cd_s:.4f} m2, trigger = {self.trigger})>"
-        )
-
-    def info(self):
-        """Prints information about the Parachute class."""
-        self.prints.all()
-
-    def all_info(self):
-        """Prints all information about the Parachute class."""
-        self.info()
-        # self.plots.all() # TODO: Parachutes still doesn't have plots
-
-    def to_dict(self, **kwargs):
-        allow_pickle = kwargs.get("allow_pickle", True)
-        trigger = self.trigger
-
-        if callable(self.trigger) and not isinstance(self.trigger, Function):
-            if allow_pickle:
-                trigger = to_hex_encode(trigger)
-            else:
-                trigger = trigger.__name__
-
-        data = {
-            "name": self.name,
-            "cd_s": self.cd_s,
-            "trigger": trigger,
-            "sampling_rate": self.sampling_rate,
-            "lag": self.lag,
-            "noise": self.noise,
-            "radius": self.radius,
-            "drag_coefficient": self.drag_coefficient,
-            "height": self.height,
-            "porosity": self.porosity,
-        }
-
-        if kwargs.get("include_outputs", False):
-            data["noise_signal"] = self.noise_signal
-            data["noise_function"] = (
-                to_hex_encode(self.noise_function)
-                if allow_pickle
-                else self.noise_function.__name__
-            )
-            data["noisy_pressure_signal"] = self.noisy_pressure_signal
-            data["clean_pressure_signal"] = self.clean_pressure_signal
-
-        return data
-
-    @classmethod
-    def from_dict(cls, data):
-        trigger = data["trigger"]
-
-        try:
-            trigger = from_hex_decode(trigger)
-        except (TypeError, ValueError):
-            pass
-
-        parachute = cls(
-            name=data["name"],
-            cd_s=data["cd_s"],
-            trigger=trigger,
-            sampling_rate=data["sampling_rate"],
-            lag=data["lag"],
-            noise=data["noise"],
-            radius=data.get("radius", None),
-            drag_coefficient=data.get("drag_coefficient", 1.4),
-            height=data.get("height", None),
-            porosity=data.get("porosity", 0.0432),
-        )
-
-        return parachute
+__all__ = ["Parachute", "HemisphericalParachute"]
diff --git a/rocketpy/rocket/parachutes/__init__.py b/rocketpy/rocket/parachutes/__init__.py
new file mode 100644
index 000000000..410d54686
--- /dev/null
+++ b/rocketpy/rocket/parachutes/__init__.py
@@ -0,0 +1,2 @@
+from .hemispherical_parachute import HemisphericalParachute
+from .parachute import Parachute
diff --git a/rocketpy/rocket/parachutes/hemispherical_parachute.py b/rocketpy/rocket/parachutes/hemispherical_parachute.py
new file mode 100644
index 000000000..25fe33dba
--- /dev/null
+++ b/rocketpy/rocket/parachutes/hemispherical_parachute.py
@@ -0,0 +1,399 @@
+import numpy as np
+
+from .parachute import Parachute
+
+
+class HemisphericalParachute(Parachute):
+    """Implements a hemispherical parachute.
+
+    Attributes
+    ----------
+    HemisphericalParachute.name : string
+        Parachute name, such as drogue and main. Has no impact in
+        simulation, as it is only used to display data in a more
+        organized matter.
+    HemisphericalParachute.parachute_type : string
+        Parachute type, such as hemispherical and parafoil.
+    HemisphericalParachute.cd_s : float
+        Drag coefficient times reference area for parachute. It has units of
+        area and must be given in squared meters.
+    HemisphericalParachute.trigger : callable, float, str
+        This parameter defines the trigger condition for the parachute ejection
+        system. It can be one of the following:
+
+        - A callable function that takes four arguments:
+          1. Freestream pressure in pascals.
+          2. Height in meters above ground level.
+          3. The state vector of the simulation, which is defined as:
+
+             `[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]`.
+
+          4. A list of sensors that are attached to the rocket. The most recent
+             measurements of the sensors are provided with the
+             ``sensor.measurement`` attribute. The sensors are listed in the same
+             order as they are added to the rocket.
+
+          The function should return ``True`` if the parachute ejection system
+          should be triggered and False otherwise. The function will be called
+          according to the specified sampling rate.
+
+        - A float value, representing an absolute height in meters. In this
+          case, the parachute will be ejected when the rocket reaches this height
+          above ground level.
+
+        - The string "apogee" which triggers the parachute at apogee, i.e.,
+          when the rocket reaches its highest point and starts descending.
+
+
+    HemisphericalParachute.triggerfunc : function
+        Trigger function created from the trigger used to evaluate the trigger
+        condition for the parachute ejection system. It is a callable function
+        that takes three arguments: Freestream pressure in Pa, Height above
+        ground level in meters, and the state vector of the simulation. The
+        returns ``True`` if the parachute ejection system should be triggered
+        and ``False`` otherwise.
+
+        .. note:
+
+            The function will be called according to the sampling rate specified.
+
+    HemisphericalParachute.sampling_rate : float
+        Sampling rate, in Hz, for the trigger function.
+    HemisphericalParachute.lag : float
+        Time, in seconds, between the parachute ejection system is triggered
+        and the parachute is fully opened.
+    HemisphericalParachute.noise : tuple, list
+        List in the format (mean, standard deviation, time-correlation).
+        The values are used to add noise to the pressure signal which is passed
+        to the trigger function. Default value is (0, 0, 0). Units are in Pa.
+    HemisphericalParachute.noise_bias : float
+        Mean value of the noise added to the pressure signal, which is
+        passed to the trigger function. Unit is in Pa.
+    HemisphericalParachute.noise_deviation : float
+        Standard deviation of the noise added to the pressure signal,
+        which is passed to the trigger function. Unit is in Pa.
+    HemisphericalParachute.noise_corr : tuple, list
+        Tuple with the correlation between noise and time.
+    HemisphericalParachute.noise_signal : list of tuple
+        List of (t, noise signal) corresponding to signal passed to
+        trigger function. Completed after running a simulation.
+    HemisphericalParachute.noisy_pressure_signal : list of tuple
+        List of (t, noisy pressure signal) that is passed to the
+        trigger function. Completed after running a simulation.
+    HemisphericalParachute.clean_pressure_signal : list of tuple
+        List of (t, clean pressure signal) corresponding to signal passed to
+        trigger function. Completed after running a simulation.
+    HemisphericalParachute.noise_signal_function : Function
+        Function of noiseSignal.
+    HemisphericalParachute.noisy_pressure_signal_function : Function
+        Function of noisy_pressure_signal.
+    HemisphericalParachute.clean_pressure_signal_function : Function
+        Function of clean_pressure_signal.
+    HemisphericalParachute.drag_coefficient : float
+        Drag coefficient of the inflated canopy shape, used only when
+        ``radius`` is not provided to estimate the parachute radius from
+        ``cd_s``: ``R = sqrt(cd_s / (drag_coefficient * pi))``. Typical
+        values: 1.4 for hemispherical canopies (default), 0.75 for flat
+        circular canopies, 1.5 for extended-skirt canopies.
+    HemisphericalParachute.radius : float
+        Length of the non-unique semi-axis (radius) of the inflated hemispherical
+        parachute in meters. If not provided at construction time, it is
+        estimated from ``cd_s`` and ``drag_coefficient``.
+    HemisphericalParachute.height : float
+        Length of the unique semi-axis (height) of the inflated hemispherical
+        parachute in meters.
+    HemisphericalParachute.porosity : float
+        Geometric porosity of the canopy (ratio of open area to total canopy
+        area), in [0, 1]. Affects only the added-mass scaling during descent;
+        it does not change ``cd_s`` (drag). The default value of 0.0432 is
+        chosen so that the resulting ``added_mass_coefficient`` equals
+        approximately 1.0 ("neutral" added-mass behavior).
+    HemisphericalParachute.added_mass_coefficient : float
+        Coefficient used to calculate the added-mass due to dragged air. It is
+        calculated from the porosity of the parachute.
+    """
+
+    def __init__(
+        self,
+        name,
+        cd_s,
+        trigger,
+        sampling_rate,
+        lag=0,
+        noise=(0, 0, 0),
+        radius=None,
+        height=None,
+        porosity=0.0432,
+        drag_coefficient=1.4,
+    ):
+        """Initializes Parachute class.
+
+        Parameters
+        ----------
+        name : string
+            Parachute name, such as drogue and main. Has no impact in
+            simulation, as it is only used to display data in a more
+            organized matter.
+        cd_s : float
+            Drag coefficient times reference area of the parachute.
+        trigger : callable, float, str
+            Defines the trigger condition for the parachute ejection system. It
+            can be one of the following:
+
+            - A callable function that takes three arguments: \
+
+                1. Freestream pressure in pascals.
+                2. Height in meters above ground level.
+                3. The state vector of the simulation, which is defined as: \
+
+                    .. code-block:: python
+
+                        u = [x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]
+
+                .. note::
+
+                    The function should return ``True`` if the parachute \
+                    ejection system should be triggered and ``False`` otherwise.
+            - A float value, representing an absolute height in meters. In this \
+                case, the parachute will be ejected when the rocket reaches this \
+                height above ground level.
+            - The string "apogee" which triggers the parachute at apogee, i.e., \
+                when the rocket reaches its highest point and starts descending.
+
+            .. note::
+
+                The function will be called according to the sampling rate specified.
+        sampling_rate : float
+            Sampling rate in which the parachute trigger will be checked at.
+            It is used to simulate the refresh rate of onboard sensors such
+            as barometers. Default value is 100. Value must be given in hertz.
+        lag : float, optional
+            Time between the parachute ejection system is triggered and the
+            parachute is fully opened. During this time, the simulation will
+            consider the rocket as flying without a parachute. Default value
+            is 0. Must be given in seconds.
+        noise : tuple, list, optional
+            List in the format (mean, standard deviation, time-correlation).
+            The values are used to add noise to the pressure signal which is
+            passed to the trigger function. Default value is ``(0, 0, 0)``.
+            Units are in Pa.
+        radius : float, optional
+            Length of the non-unique semi-axis (radius) of the inflated
+            hemispherical parachute. If not provided, it is estimated from
+            ``cd_s`` and ``drag_coefficient`` using:
+            ``radius = sqrt(cd_s / (drag_coefficient * pi))``.
+            Units are in meters.
+        height : float, optional
+            Length of the unique semi-axis (height) of the inflated hemispherical
+            parachute. Default value is the radius of the parachute.
+            Units are in meters.
+        porosity : float, optional
+            Geometric porosity of the canopy (ratio of open area to total
+            canopy area), in [0, 1]. Affects only the added-mass scaling
+            during descent; it does not change ``cd_s`` (drag). The default
+            value of 0.0432 is chosen so that the resulting
+            ``added_mass_coefficient`` equals approximately 1.0 ("neutral"
+            added-mass behavior).
+        drag_coefficient : float, optional
+            Drag coefficient of the inflated canopy shape, used only when
+            ``radius`` is not provided. It relates the aerodynamic ``cd_s``
+            to the physical canopy area via
+            ``cd_s = drag_coefficient * pi * radius**2``. Typical values:
+
+            - **1.4** — hemispherical canopy (default, NASA SP-8066)
+            - **0.75** — flat circular canopy
+            - **1.5** — extended-skirt canopy
+
+            Has no effect when ``radius`` is explicitly provided.
+        """
+
+        parachute_type = "hemispherical"
+        super().__init__(
+            name=name,
+            parachute_type=parachute_type,
+            trigger=trigger,
+            sampling_rate=sampling_rate,
+            lag=lag,
+            noise=noise,
+        )
+        self.cd_s = cd_s
+        self.trigger = trigger
+        self.drag_coefficient = drag_coefficient
+        self.porosity = porosity
+
+        # Initialize derived attributes
+        self.radius = self.__resolve_radius(radius, cd_s, drag_coefficient)
+        self.height = self.__resolve_height(height, self.radius)
+        self.added_mass_coefficient = self.__compute_added_mass_coefficient(
+            self.porosity
+        )
+
+    def __resolve_radius(self, radius, cd_s, drag_coefficient):
+        """Resolves parachute radius from input or aerodynamic relation."""
+        if radius is not None:
+            return radius
+
+        # cd_s = Cd * S = Cd * pi * R^2  =>  R = sqrt(cd_s / (Cd * pi))
+        return np.sqrt(cd_s / (drag_coefficient * np.pi))
+
+    def __resolve_height(self, height, radius):
+        """Resolves parachute height defaulting to radius when not provided."""
+        return height or radius
+
+    def __compute_added_mass_coefficient(self, porosity):
+        """Computes the added-mass coefficient from canopy porosity."""
+        return 1.068 * (
+            1 - 1.465 * porosity - 0.25975 * porosity**2 + 1.2626 * porosity**3
+        )
+
+    def add_information_to_flight(self, flight_obj, additional_info):
+        """Adds parachute information to flight"""
+        drag = additional_info["drag"]
+        t = additional_info["t"]
+        if self.name not in flight_obj.parachutes_info.keys():
+            flight_obj.parachutes_info[self.name] = {"drag": [], "t": []}
+            flight_obj.parachutes_info[self.name]["drag"].append(drag)
+            flight_obj.parachutes_info[self.name]["t"].append(t)
+        else:
+            # LSODA did not accept last solution, we replace it
+            if t == flight_obj.parachutes_info[self.name]["t"][-1]:
+                flight_obj.parachutes_info[self.name]["drag"][-1] = drag
+                flight_obj.parachutes_info[self.name]["t"][-1] = t
+            else:
+                flight_obj.parachutes_info[self.name]["drag"].append(drag)
+                flight_obj.parachutes_info[self.name]["t"].append(t)
+
+    # pylint: disable=too-many-locals, too-many-statements
+    def u_dot(self, t, u, flight_information, post_processing=False):
+        """Calculates derivative of u state vector with respect to time
+        when rocket is flying under parachute. Each parachute type has
+
+
+        Parameters
+        ----------
+        t : float
+            Time in seconds
+        u : list
+            State vector defined by u = [x, y, z, vx, vy, vz, e0, e1,
+            e2, e3, omega1, omega2, omega3].
+        flight_information : dictionary
+            A dictionary containing additional information used in
+            the parachute equations of motion. Examples are
+            Environment and Rocket data
+        post_processing : bool, optional
+            If True, adds flight data information directly to self
+            variables such as self.angle_of_attack. Default is False.
+
+        Return
+        ------
+        u_dot : dict
+            A dictionary containing two or three keys
+            1) state: State vector which depends on the parachute model.
+            2) additional_information: information as dict that is added
+            to the  'parachutes_info' attribute in the Flight class.
+            3) post_processing_information: State vector containing
+            post processing information.
+
+        """
+        # Get relevant state data
+        z, vx, vy, vz = u[2:6]
+
+        env = flight_information["env"]
+        rocket = flight_information["rocket"]
+
+        # Get atmospheric data
+        rho = env.density.get_value_opt(z)
+        wind_velocity_x = env.wind_velocity_x.get_value_opt(z)
+        wind_velocity_y = env.wind_velocity_y.get_value_opt(z)
+
+        # Get the mass of the rocket
+        mp = rocket.dry_mass
+
+        # Calculate added mass
+        ma = (
+            self.added_mass_coefficient
+            * rho
+            * (2 / 3)
+            * np.pi
+            * self.radius**2
+            * self.height
+        )
+
+        # Calculate freestream speed
+        freestream_x = vx - wind_velocity_x
+        freestream_y = vy - wind_velocity_y
+        freestream_z = vz
+        free_stream_speed = (freestream_x**2 + freestream_y**2 + freestream_z**2) ** 0.5
+
+        # Determine drag force
+        pseudo_drag = -0.5 * rho * self.cd_s * free_stream_speed
+        Dx = pseudo_drag * freestream_x
+        Dy = pseudo_drag * freestream_y
+        Dz = pseudo_drag * freestream_z
+        total_drag = np.sqrt(Dx**2 + Dy**2 + Dz**2)
+        ax = Dx / (mp + ma)
+        ay = Dy / (mp + ma)
+        az = (Dz - mp * env.gravity.get_value_opt(z)) / (mp + ma)
+
+        # Add coriolis acceleration
+        _, w_earth_y, w_earth_z = env.earth_rotation_vector
+        ax -= 2 * (vz * w_earth_y - vy * w_earth_z)
+        ay -= 2 * (vx * w_earth_z)
+        az -= 2 * (-vx * w_earth_y)
+
+        additional_info = {
+            "t": t,
+            "drag": total_drag,
+        }
+        output = {
+            "state": [vx, vy, vz, ax, ay, az, 0, 0, 0, 0, 0, 0, 0],
+            "additional_info": additional_info,
+        }
+
+        if post_processing:
+            output["post_processing_information"] = [
+                t,
+                ax,
+                ay,
+                az,
+                0,
+                0,
+                0,
+                Dx,
+                Dy,
+                Dz,
+                0,
+                0,
+                0,
+                0,
+            ]
+        return output
+
+    # serialization methods
+    def to_dict(self, **kwargs):
+        data = super().to_dict(**kwargs)
+        data.update(
+            {
+                "cd_s": self.cd_s,
+                "radius": self.radius,
+                "drag_coefficient": self.drag_coefficient,
+                "height": self.height,
+                "porosity": self.porosity,
+            }
+        )
+        return data
+
+    @classmethod
+    def from_dict(cls, data):
+        return cls(
+            name=data["name"],
+            cd_s=data["cd_s"],
+            trigger=cls._decode_trigger(data["trigger"]),
+            sampling_rate=data["sampling_rate"],
+            lag=data["lag"],
+            noise=data["noise"],
+            radius=data.get("radius", None),
+            drag_coefficient=data.get("drag_coefficient", 1.4),
+            height=data.get("height", None),
+            porosity=data.get("porosity", 0.0432),
+        )
diff --git a/rocketpy/rocket/parachutes/parachute.py b/rocketpy/rocket/parachutes/parachute.py
new file mode 100644
index 000000000..a9b2c290d
--- /dev/null
+++ b/rocketpy/rocket/parachutes/parachute.py
@@ -0,0 +1,412 @@
+from abc import ABC, abstractmethod
+from inspect import signature
+
+import numpy as np
+
+from rocketpy.tools import from_hex_decode, to_hex_encode
+
+from ...mathutils.function import Function
+from ...prints.parachute_prints import _ParachutePrints
+
+
+class Parachute(ABC):
+    """Abstract class to specify characteristics and useful operations for
+    parachutes. Cannot be instantiated.
+
+    Attributes
+    ----------
+    Parachute.name : string
+        Parachute name, such as drogue and main. Has no impact in
+        simulation, as it is only used to display data in a more
+        organized matter.
+    Parachute.parachute_type : string
+        Parachute type, such as hemispherical and parafoil.
+    Parachute.trigger : callable, float, str
+        This parameter defines the trigger condition for the parachute ejection
+        system. It can be one of the following:
+
+        - A callable function that can take 3, 4, or 5 arguments:
+
+          **3 arguments**:
+            1. Freestream pressure in pascals.
+            2. Height in meters above ground level.
+            3. The state vector: ``[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]``
+
+          **4 arguments** (sensors OR acceleration):
+            1. Freestream pressure in pascals.
+            2. Height in meters above ground level.
+            3. The state vector.
+            4. Either:
+               - ``sensors``: List of sensor objects attached to the rocket, OR
+               - ``u_dot``: State derivative including accelerations at indices [3:6]
+
+          **5 arguments** (sensors AND acceleration):
+            1. Freestream pressure in pascals.
+            2. Height in meters above ground level.
+            3. The state vector.
+            4. ``sensors``: List of sensor objects.
+            5. ``u_dot``: State derivative with accelerations ``[vx, vy, vz, ax, ay, az, ...]``
+
+          The function should return ``True`` to trigger deployment, ``False`` otherwise.
+          The function will be called according to the specified sampling rate.
+
+        - A float value, representing an absolute height in meters. In this
+          case, the parachute will be ejected when the rocket reaches this height
+          above ground level while descending.
+
+        - The string "apogee" which triggers the parachute at apogee, i.e.,
+          when the rocket reaches its highest point and starts descending.
+
+
+    Parachute.triggerfunc : function
+        Trigger function created from the trigger used to evaluate the trigger
+        condition for the parachute ejection system. It is a callable function
+        that takes five arguments: Freestream pressure in Pa, Height above
+        ground level in meters, the state vector, sensors list, and u_dot.
+        Returns ``True`` if the parachute ejection system should be triggered
+        and ``False`` otherwise.
+
+        .. note::
+
+            The function will be called according to the sampling rate specified.
+
+    Parachute.sampling_rate : float
+        Sampling rate, in Hz, for the trigger function.
+    Parachute.lag : float
+        Time, in seconds, between the parachute ejection system is triggered
+        and the parachute is fully opened.
+    Parachute.noise : tuple, list
+        List in the format (mean, standard deviation, time-correlation).
+        The values are used to add noise to the pressure signal which is passed
+        to the trigger function. Default value is (0, 0, 0). Units are in Pa.
+    Parachute.noise_bias : float
+        Mean value of the noise added to the pressure signal, which is
+        passed to the trigger function. Unit is in Pa.
+    Parachute.noise_deviation : float
+        Standard deviation of the noise added to the pressure signal,
+        which is passed to the trigger function. Unit is in Pa.
+    Parachute.noise_corr : tuple, list
+        Tuple with the correlation between noise and time.
+    Parachute.noise_signal : list of tuple
+        List of (t, noise signal) corresponding to signal passed to
+        trigger function. Completed after running a simulation.
+    Parachute.noisy_pressure_signal : list of tuple
+        List of (t, noisy pressure signal) that is passed to the
+        trigger function. Completed after running a simulation.
+    Parachute.clean_pressure_signal : list of tuple
+        List of (t, clean pressure signal) corresponding to signal passed to
+        trigger function. Completed after running a simulation.
+    Parachute.noise_signal_function : Function
+        Function of noiseSignal.
+    Parachute.noisy_pressure_signal_function : Function
+        Function of noisy_pressure_signal.
+    Parachute.clean_pressure_signal_function : Function
+        Function of clean_pressure_signal.
+    """
+
+    def __init__(
+        self,
+        name,
+        parachute_type,
+        trigger,
+        sampling_rate,
+        lag=0,
+        noise=(0, 0, 0),
+    ):
+        """Initializes Parachute class.
+
+        Parameters
+        ----------
+        name : string
+            Parachute name, such as drogue and main. Has no impact in
+            simulation, as it is only used to display data in a more
+            organized matter.
+        parachute_type : string
+            Parachute type, such as hemispherical and parafoil.
+        trigger : callable, float, str
+            Defines the trigger condition for the parachute ejection system. It
+            can be one of the following:
+
+            - A callable function that takes three or four arguments: \
+
+                1. Freestream pressure in pascals.
+                2. Height in meters above ground level.
+                3. The state vector of the simulation, which is defined as: \
+
+                    .. code-block:: python
+
+                        u = [x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]
+
+                4. (optional) A list of sensors attached to the rocket.
+
+                .. note::
+
+                    The function should return ``True`` if the parachute \
+                    ejection system should be triggered and ``False`` otherwise.
+            - A float value, representing an absolute height in meters. In this \
+                case, the parachute will be ejected when the rocket reaches this \
+                height above ground level.
+            - The string "apogee" which triggers the parachute at apogee, i.e., \
+                when the rocket reaches its highest point and starts descending.
+
+            .. note::
+
+                The function will be called according to the sampling rate specified.
+        sampling_rate : float
+            Sampling rate in which the parachute trigger will be checked at.
+            It is used to simulate the refresh rate of onboard sensors such
+            as barometers. Default value is 100. Value must be given in hertz.
+        lag : float, optional
+            Time between the parachute ejection system is triggered and the
+            parachute is fully opened. During this time, the simulation will
+            consider the rocket as flying without a parachute. Default value
+            is 0. Must be given in seconds.
+        noise : tuple, list, optional
+            List in the format (mean, standard deviation, time-correlation).
+            The values are used to add noise to the pressure signal which is
+            passed to the trigger function. Default value is ``(0, 0, 0)``.
+            Units are in Pa.
+        """
+
+        # Save arguments as attributes
+        self.name = name
+        self.parachute_type = parachute_type
+        self.trigger = trigger
+        self.sampling_rate = sampling_rate
+        self.lag = lag
+        self.noise = noise
+        self.__init_noise(noise)
+        self.__evaluate_trigger_function(trigger)
+
+        # Prints and plots
+        self.prints = _ParachutePrints(self)
+
+    def __init_noise(self, noise):
+        """Initializes all noise-related attributes.
+
+        Parameters
+        ----------
+        noise : tuple, list
+            List in the format (mean, standard deviation, time-correlation).
+        """
+        self.noise_signal = [[-1e-6, np.random.normal(noise[0], noise[1])]]
+        self.noisy_pressure_signal = []
+        self.clean_pressure_signal = []
+        self.noise_bias = noise[0]
+        self.noise_deviation = noise[1]
+        self.noise_corr = (noise[2], (1 - noise[2] ** 2) ** 0.5)
+        self.clean_pressure_signal_function = Function(0)
+        self.noisy_pressure_signal_function = Function(0)
+        self.noise_signal_function = Function(0)
+        alpha, beta = self.noise_corr
+        self.noise_function = lambda: (
+            alpha * self.noise_signal[-1][1]
+            + beta * np.random.normal(noise[0], noise[1])
+        )
+
+    def __evaluate_trigger_function(self, trigger):  # pylint: disable=too-many-statements
+        """This is used to set the triggerfunc attribute that will be used to
+        interact with the Flight class.
+
+        Notes
+        -----
+        The resulting triggerfunc always has signature (p, h, y, sensors, u_dot)
+        so Flight can pass both sensors and u_dot when needed.
+        """
+        # pylint: disable=unused-argument, function-redefined
+
+        # Helper to wrap any callable to the internal (p, h, y, sensors, u_dot) API
+        def _make_wrapper(fn):
+            params = list(signature(fn).parameters.keys())
+            num_params = len(params)
+            fn_name = getattr(fn, "__name__", repr(fn))
+
+            # Validate arity up-front so a malformed trigger fails at
+            # construction time rather than mid-simulation.
+            if num_params < 3:
+                raise TypeError(
+                    f"Trigger function '{fn_name}' has unsupported signature: "
+                    f"expected 3, 4, or 5+ arguments, got {num_params}. "
+                    "Please check the function definition."
+                )
+
+            # A 4-argument trigger is ambiguous: the 4th argument may be either
+            # the sensors list or the acceleration (u_dot). Disambiguate by the
+            # parameter name. A 5+ argument trigger follows the positional
+            # contract (p, h, y, sensors, u_dot), so it always receives u_dot.
+            fourth_is_udot = num_params == 4 and params[3].lower() in (
+                "u_dot",
+                "udot",
+                "acc",
+                "acceleration",
+            )
+
+            # Tell Flight whether it must compute u_dot for this trigger. Gate on
+            # ARITY (not parameter names) for 5+ arg triggers so documented,
+            # positionally-correct triggers with descriptive parameter names
+            # still receive a valid u_dot instead of None.
+            expects_udot = num_params >= 5 or fourth_is_udot
+
+            def wrapper(p, h, y, sensors, u_dot):
+                if num_params == 3:
+                    return fn(p, h, y)
+                if num_params == 4:
+                    if fourth_is_udot:
+                        return fn(p, h, y, u_dot)
+                    return fn(p, h, y, sensors)
+                # num_params >= 5: positional contract (p, h, y, sensors, u_dot)
+                return fn(p, h, y, sensors, u_dot)
+
+            # attach metadata so Flight can decide whether to compute u_dot
+            wrapper._expects_udot = expects_udot
+            return wrapper
+
+        # Callable provided by user
+        if callable(trigger):
+            self.triggerfunc = _make_wrapper(trigger)
+            return
+
+        # Numeric altitude trigger
+        if isinstance(trigger, (int, float)):
+
+            def triggerfunc(p, h, y, sensors, u_dot):  # pylint: disable=unused-argument
+                # p = pressure considering parachute noise signal
+                # h = height above ground level considering parachute noise signal
+                # y = [x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]
+                return y[5] < 0 and h < trigger
+
+            triggerfunc._expects_udot = False
+            self.triggerfunc = triggerfunc
+            return
+
+        # Special case: "apogee"
+        if isinstance(trigger, str) and trigger.lower() == "apogee":
+
+            def triggerfunc(p, h, y, sensors, u_dot):  # pylint: disable=unused-argument
+                return y[5] < 0
+
+            triggerfunc._expects_udot = False
+            self.triggerfunc = triggerfunc
+            return
+
+        # If we reach this point, the trigger is invalid
+        raise ValueError(
+            f"Unable to set the trigger function for parachute '{self.name}'. "
+            + "Trigger must be a callable, a float value or one of the strings "
+            + "('apogee'). "
+            + "See the Parachute class documentation for more information."
+        )
+
+    def __str__(self):
+        """Returns a string representation of the Parachute class.
+
+        Returns
+        -------
+        string
+            String representation of Parachute class. It is human readable.
+        """
+        return f"Parachute {self.name.title()} of type {self.parachute_type}"
+
+    def __repr__(self):
+        """Representation method for the class, useful when debugging."""
+        return (
+            f"<Parachute {self.name} of type {self.parachute_type} "
+            + f"(lag = {self.lag:.4f} s, trigger = {self.trigger})>"
+        )
+
+    def info(self):
+        """Prints information about the Parachute class."""
+        self.prints.all()
+
+    def all_info(self):
+        """Prints all information about the Parachute class."""
+        self.info()
+
+    @abstractmethod
+    def add_information_to_flight(self, flight_obj, additional_info):
+        """Adds parachute information to flight"""
+
+    @abstractmethod
+    def u_dot(self, t, u, flight_information, post_processing=False):
+        """Calculates derivative of u state vector with respect to time
+        when rocket is flying under parachute. Each parachute type has
+
+
+        Parameters
+        ----------
+        t : float
+            Time in seconds
+        u : list
+            State vector defined by u = [x, y, z, vx, vy, vz, e0, e1,
+            e2, e3, omega1, omega2, omega3].
+        flight_information : dictionary
+            A dictionary containing additional information used in
+            the parachute equations of motion. Examples are
+            Environment and Rocket data
+        post_processing : bool, optional
+            If True, adds flight data information directly to self
+            variables such as self.angle_of_attack. Default is False.
+
+        Return
+        ------
+        u_dot : dict
+            A dictionary containing two or three keys
+            1) state: State vector which depends on the parachute model.
+            2) additional_information: information as dict that is added
+            to the  'parachutes_info' attribute in the Flight class.
+            3) post_processing_information: State vector containing
+            post processing information.
+
+        """
+
+    def to_dict(self, **kwargs):
+        """Serializes the fields shared by every parachute model. Subclasses
+        should call ``super().to_dict(**kwargs)`` and add their model-specific
+        attributes to the returned dictionary."""
+        allow_pickle = kwargs.get("allow_pickle", True)
+        trigger = self.trigger
+
+        if callable(self.trigger) and not isinstance(self.trigger, Function):
+            if allow_pickle:
+                trigger = to_hex_encode(trigger)
+            else:
+                trigger = trigger.__name__
+
+        data = {
+            "name": self.name,
+            "parachute_type": self.parachute_type,
+            "trigger": trigger,
+            "sampling_rate": self.sampling_rate,
+            "lag": self.lag,
+            "noise": self.noise,
+        }
+
+        if kwargs.get("include_outputs", False):
+            data["noise_signal"] = self.noise_signal
+            data["noise_function"] = (
+                to_hex_encode(self.noise_function)
+                if allow_pickle
+                else self.noise_function.__name__
+            )
+            data["noisy_pressure_signal"] = self.noisy_pressure_signal
+            data["clean_pressure_signal"] = self.clean_pressure_signal
+
+        return data
+
+    @staticmethod
+    def _decode_trigger(trigger):
+        """Decodes a (possibly hex-encoded) serialized trigger back into a
+        callable, leaving numeric/string triggers untouched."""
+        try:
+            return from_hex_decode(trigger)
+        except (TypeError, ValueError):
+            return trigger
+
+    @classmethod
+    @abstractmethod
+    def from_dict(cls, data):
+        """Reconstructs a parachute from a serialized dictionary.
+
+        Each concrete model must implement this using its own constructor,
+        since the required arguments differ per model. The shared
+        ``_decode_trigger`` helper handles the ``trigger`` field."""
diff --git a/rocketpy/rocket/rocket.py b/rocketpy/rocket/rocket.py
index e3692d2e8..2ed7fce47 100644
--- a/rocketpy/rocket/rocket.py
+++ b/rocketpy/rocket/rocket.py
@@ -1,12 +1,20 @@
 import csv
 import inspect
+import logging
 import math
+import numbers
 import warnings
 from typing import Iterable
+from warnings import warn
 
 import numpy as np
 
 from rocketpy.control.controller import _Controller
+from rocketpy.exceptions import (
+    InvalidInertiaError,
+    InvalidParameterError,
+    UnstableRocketWarning,
+)
 from rocketpy.mathutils.function import Function
 from rocketpy.mathutils.vector_matrix import Matrix, Vector
 from rocketpy.motors.empty_motor import EmptyMotor
@@ -21,16 +29,22 @@
     Tail,
     TrapezoidalFins,
 )
+from rocketpy.rocket.aero_surface.fins.elliptical_fin import EllipticalFin
+from rocketpy.rocket.aero_surface.fins.free_form_fin import FreeFormFin
 from rocketpy.rocket.aero_surface.fins.free_form_fins import FreeFormFins
+from rocketpy.rocket.aero_surface.fins.trapezoidal_fin import TrapezoidalFin
 from rocketpy.rocket.aero_surface.generic_surface import GenericSurface
 from rocketpy.rocket.components import Components
-from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.parachutes.hemispherical_parachute import HemisphericalParachute
+from rocketpy.rocket.parachutes.parachute import Parachute
 from rocketpy.tools import (
     deprecated,
     find_obj_from_hash,
     parallel_axis_theorem_from_com,
 )
 
+logger = logging.getLogger(__name__)
+
 
 # pylint: disable=too-many-instance-attributes, too-many-public-methods, too-many-instance-attributes
 class Rocket:
@@ -308,6 +322,29 @@ def __init__(  # pylint: disable=too-many-statements
                     + '"tail_to_nose" and "nose_to_tail".'
                 )
 
+        # Validate inputs. Accept Python and NumPy numeric scalars for
+        # radius/mass, and any length-3 or length-6 sequence (tuple, list or
+        # numpy array) for inertia, matching the permissive behavior of earlier
+        # versions (numpy inputs are common when computing inertia tensors).
+        if not isinstance(radius, numbers.Real) or radius <= 0:
+            raise InvalidParameterError(
+                f"Rocket radius must be a positive number, got {radius!r}."
+            )
+        if not isinstance(mass, numbers.Real) or mass <= 0:
+            raise InvalidParameterError(
+                f"Rocket mass must be a positive number, got {mass!r}."
+            )
+        try:
+            inertia_length = len(inertia)
+        except TypeError:
+            inertia_length = None
+        if isinstance(inertia, str) or inertia_length not in (3, 6):
+            raise InvalidInertiaError(
+                "Inertia must be a length-3 (I_11, I_22, I_33) or length-6 "
+                "(I_11, I_22, I_33, I_12, I_13, I_23) sequence, "
+                f"got {inertia!r}."
+            )
+
         # Define rocket inertia attributes in SI units
         self.mass = mass
         inertia = (*inertia, 0, 0, 0) if len(inertia) == 3 else inertia
@@ -475,7 +512,7 @@ def evaluate_total_mass(self):
         """
         # Make sure there is a motor associated with the rocket
         if self.motor is None:
-            print("Please associate this rocket with a motor!")
+            logger.warning("Please associate this rocket with a motor!")
             return False
 
         self.total_mass = self.mass + self.motor.total_mass
@@ -495,7 +532,7 @@ def evaluate_dry_mass(self):
         """
         # Make sure there is a motor associated with the rocket
         if self.motor is None:
-            print("Please associate this rocket with a motor!")
+            logger.warning("Please associate this rocket with a motor!")
             return False
 
         self.dry_mass = self.mass + self.motor.dry_mass
@@ -578,7 +615,7 @@ def evaluate_reduced_mass(self):
         # TODO: add tests for reduced_mass values
         # Make sure there is a motor associated with the rocket
         if self.motor is None:
-            print("Please associate this rocket with a motor!")
+            logger.warning("Please associate this rocket with a motor!")
             return False
 
         # Get nicknames
@@ -661,14 +698,20 @@ def __evaluate_single_surface_cp_to_cdm(self, surface, position):
         """Calculates the relative position of each aerodynamic surface
         center of pressure to the rocket's center of dry mass in Body Axes
         Coordinate System."""
-        pos = Vector(
+        # position of the surfaces coordinate system origin in body frame
+        pos_origin = Vector(
             [
-                (position.x - self.cm_eccentricity_x) * self._csys - surface.cpx,
-                (position.y - self.cm_eccentricity_y) - surface.cpy,
-                (position.z - self.center_of_dry_mass_position) * self._csys
-                - surface.cpz,
+                (position.x - self.cm_eccentricity_x) * self._csys,
+                (position.y - self.cm_eccentricity_y),
+                (position.z - self.center_of_dry_mass_position) * self._csys,
             ]
         )
+        # position of the center of pressure in body frame
+        pos = (
+            surface._rotation_surface_to_body
+            @ Vector([surface.cpx, surface.cpy, surface.cpz])
+            + pos_origin
+        )  # TODO: this should be recomputed whenever cant angle changes for fin
         self.surfaces_cp_to_cdm[surface] = pos
 
     def evaluate_stability_margin(self):
@@ -727,6 +770,45 @@ def evaluate_static_margin(self):
         )
         return self.static_margin
 
+    def warn_if_unstable(self):
+        """Warn if the rocket is aerodynamically unstable at motor ignition.
+
+        Emits an :class:`UnstableRocketWarning` when the static margin at
+        ``t=0`` is negative. This is meant to be checked once the rocket is
+        fully assembled (e.g. when a :class:`Flight` is created), not during
+        incremental construction, so that partially-built-but-ultimately-stable
+        rockets do not raise spurious warnings.
+
+        The check is skipped when ``GenericSurface`` instances are present:
+        their lift coefficient derivative is not accounted for in
+        ``evaluate_center_of_pressure``, so the computed static margin does not
+        reflect their contribution and cannot be trusted for this check.
+
+        Returns
+        -------
+        bool
+            ``True`` if a warning was emitted, ``False`` otherwise.
+        """
+        has_generic_surface = any(
+            isinstance(aero_surface, GenericSurface)
+            for aero_surface, _position in self.aerodynamic_surfaces
+        )
+        if has_generic_surface:
+            return False
+
+        initial_static_margin = self.static_margin.get_value_opt(0)
+        if initial_static_margin < 0:
+            warnings.warn(
+                f"The rocket has a negative static margin "
+                f"({initial_static_margin:.2f} cal) at motor ignition (t=0), "
+                "indicating an aerodynamically unstable configuration. Check the "
+                "placement of fins and nose cone relative to the center of mass.",
+                UnstableRocketWarning,
+                stacklevel=2,
+            )
+            return True
+        return False
+
     def evaluate_dry_inertias(self):
         """Calculates and returns the rocket's dry inertias relative to
         the rocket's center of dry mass. The inertias are saved and returned
@@ -1027,9 +1109,9 @@ def add_motor(self, motor, position):  # pylint: disable=too-many-statements
         if hasattr(self, "motor"):
             # pylint: disable=access-member-before-definition
             if not isinstance(self.motor, EmptyMotor):
-                print(
+                logger.warning(
                     "Only one motor per rocket is currently supported. "
-                    + "Overwriting previous motor."
+                    "Overwriting previous motor."
                 )
         self.motor = motor
         self.motor_position = position
@@ -1066,11 +1148,20 @@ def __add_single_surface(self, surface, position):
         """Adds a single aerodynamic surface to the rocket. Makes checks for
         rail buttons case, and position type.
         """
-        position = (
-            Vector([0, 0, position])
-            if not isinstance(position, (Vector, tuple, list))
-            else Vector(position)
-        )
+        if isinstance(surface, (TrapezoidalFin, EllipticalFin, FreeFormFin)):
+            # TODO: the leading edge position should be recomputed whenever cant
+            # angle of the fin changes, but currently it is only computed at the
+            # moment the fin is added to the rocket. Detecting when the cant
+            # angle changes is hard, because it is a parameter of the fin, while
+            # the leading edge position is only defined on the rocket
+            position = surface._compute_leading_edge_position(position, self._csys)
+        else:
+            position = (
+                Vector([0, 0, position])
+                if not isinstance(position, (Vector, tuple, list))
+                else Vector(position)
+            )
+
         if isinstance(surface, RailButtons):
             self.rail_buttons = Components()
             self.rail_buttons.add(surface, position)
@@ -1085,17 +1176,23 @@ def add_surfaces(self, surfaces, positions):
 
         Parameters
         ----------
-        surfaces : list, AeroSurface, NoseCone, TrapezoidalFins, EllipticalFins, Tail, RailButtons
+        surfaces : list[AeroSurface], AeroSurface
             Aerodynamic surface to be added to the rocket. Can be a list of
             AeroSurface if more than one surface is to be added.
-        positions : int, float, list, tuple, Vector
-            Position, in m, of the aerodynamic surface's center of pressure
-            relative to the user defined rocket coordinate system.
-            If a list is passed, it will correspond to the position of each item
-            in the surfaces list.
-            For NoseCone type, position is relative to the nose cone tip.
-            For Fins type, position is relative to the point belonging to
-            the root chord which is highest in the rocket coordinate system.
+        positions : int, float, tuple, list, Vector
+            Position(s) of the aerodynamic surface's reference point. Can be:
+
+            - a single number (int or float) giving the z-coordinate along
+              the rocket axis.
+            - a sequence of three numbers (x, y, z) representing the full
+              position in the user-defined coordinate system.
+
+            If passing multiple surfaces, provide a list of positions matching
+            each surface in order.
+            For NoseCone type, position is the tip coordinate along the axis.
+            For Fins type, position refers to the z-coordinate of the root
+            chord leading-edge point closest to the nose cone, before any
+            cant-angle offset is considered.
             For Tail type, position is relative to the point belonging to the
             tail which is highest in the rocket coordinate system.
             For RailButtons type, position is relative to the lower rail button.
@@ -1108,10 +1205,18 @@ def add_surfaces(self, surfaces, positions):
         -------
         None
         """
-        try:
+        if isinstance(surfaces, Iterable):
+            if isinstance(positions, Iterable):
+                if len(surfaces) != len(positions):
+                    raise ValueError(
+                        "The number of surfaces and positions must be the same."
+                    )
+            else:
+                positions = [positions] * len(surfaces)
+
             for surface, position in zip(surfaces, positions):
                 self.__add_single_surface(surface, position)
-        except TypeError:
+        else:
             self.__add_single_surface(surfaces, positions)
 
         self.evaluate_center_of_pressure()
@@ -1285,10 +1390,10 @@ def add_trapezoidal_fins(
         tip_chord : int, float
             Fin tip chord in meters.
         position : int, float
-            Fin set position relative to the rocket's coordinate system.
-            By fin set position, understand the point belonging to the root
-            chord which is highest in the rocket coordinate system (i.e.
-            the point closest to the nose cone tip).
+            Fin set position in the z coordinate of the user defined rocket
+            coordinate system. By fin set position, understand the point
+            belonging to the root chord which is highest in the rocket
+            coordinate system (i.e. the point closest to the nose cone tip).
 
             See Also
             --------
@@ -1334,6 +1439,15 @@ def add_trapezoidal_fins(
         fin_set : TrapezoidalFins
             Fin set object created.
         """
+        if n <= 2:
+            warnings.warn(
+                "Fin sets with 2 or fewer fins assume a symmetric, evenly-spaced "
+                "configuration and may not accurately capture asymmetric forces. "
+                "For 1 or 2 fins, consider creating individual fin objects "
+                "(e.g. TrapezoidalFin) and adding them with add_surfaces.",
+                UserWarning,
+                stacklevel=2,
+            )
 
         # Modify radius if not given, use rocket radius, otherwise use given.
         radius = radius if radius is not None else self.radius
@@ -1381,10 +1495,10 @@ def add_elliptical_fins(
         span : int, float
             Fin span in meters.
         position : int, float
-            Fin set position relative to the rocket's coordinate system. By fin
-            set position, understand the point belonging to the root chord which
-            is highest in the rocket coordinate system (i.e. the point
-            closest to the nose cone tip).
+            Fin set position in the z coordinate of the user defined rocket
+            coordinate system. By fin set position, understand the point
+            belonging to the root chord which is highest in the rocket
+            coordinate system (i.e. the point closest to the nose cone tip).
 
             See Also
             --------
@@ -1420,6 +1534,16 @@ def add_elliptical_fins(
         fin_set : EllipticalFins
             Fin set object created.
         """
+        if n <= 2:
+            warnings.warn(
+                "Fin sets with 2 or fewer fins assume a symmetric, evenly-spaced "
+                "configuration and may not accurately capture asymmetric forces. "
+                "For 1 or 2 fins, consider creating individual fin objects "
+                "(e.g. TrapezoidalFin) and adding them with add_surfaces.",
+                UserWarning,
+                stacklevel=2,
+            )
+
         radius = radius if radius is not None else self.radius
         fin_set = EllipticalFins(n, root_chord, span, radius, cant_angle, airfoil, name)
         self.add_surfaces(fin_set, position)
@@ -1451,10 +1575,10 @@ def add_free_form_fins(
             The shape will be interpolated between the points, in the order
             they are given. The last point connects to the first point.
         position : int, float
-            Fin set position relative to the rocket's coordinate system.
-            By fin set position, understand the point belonging to the root
-            chord which is highest in the rocket coordinate system (i.e.
-            the point closest to the nose cone tip).
+            Fin set position in the z coordinate of the user defined rocket
+            coordinate system. By fin set position, understand the point
+            belonging to the root chord which is highest in the rocket
+            coordinate system (i.e. the point closest to the nose cone tip).
 
             See Also
             --------
@@ -1486,6 +1610,15 @@ def add_free_form_fins(
         fin_set : FreeFormFins
             Fin set object created.
         """
+        if n <= 2:
+            warnings.warn(
+                "Fin sets with 2 or fewer fins assume a symmetric, evenly-spaced "
+                "configuration and may not accurately capture asymmetric forces. "
+                "For 1 or 2 fins, consider creating individual fin objects "
+                "(e.g. TrapezoidalFin) and adding them with add_surfaces.",
+                UserWarning,
+                stacklevel=2,
+            )
 
         # Modify radius if not given, use rocket radius, otherwise use given.
         radius = radius if radius is not None else self.radius
@@ -1505,9 +1638,9 @@ def add_free_form_fins(
 
     def add_parachute(
         self,
-        name,
-        cd_s,
-        trigger,
+        name=None,
+        cd_s=None,
+        trigger=None,
         sampling_rate=100,
         lag=0,
         noise=(0, 0, 0),
@@ -1515,12 +1648,16 @@ def add_parachute(
         height=None,
         porosity=0.0432,
         drag_coefficient=1.4,
+        parachute=None,
     ):
-        """Creates a new parachute, storing its parameters such as
-        opening delay, drag coefficients and trigger function.
+        """Adds parachute to the rocket parachute list
 
         Parameters
         ----------
+        parachute : object with parent class Parachute | None
+            The parachute object to be added to the rocket. Default is
+            none for backwards compatibility. In future versions, it
+            will be required to pass a valid object.
         name : string
             Parachute name, such as drogue and main. Has no impact in
             simulation, as it is only used to display data in a more
@@ -1597,26 +1734,54 @@ def add_parachute(
 
         Returns
         -------
-        parachute : Parachute
-            Parachute containing trigger, sampling_rate, lag, cd_s, noise,
+        parachute : Parachute | None
+            If the parachute argument is not None, nothing is returned.
+            If the parachute argument is None, then it returns a
+            Parachute object containing trigger, sampling_rate, lag, cd_s, noise,
             radius, drag_coefficient, height, porosity and name. Furthermore,
             it stores clean_pressure_signal, noise_signal and
             noisyPressureSignal which are filled in during Flight simulation.
+            Returning a Parachute object is deprecated and will be removed
+            in future versions.
         """
-        parachute = Parachute(
-            name,
-            cd_s,
-            trigger,
-            sampling_rate,
-            lag,
-            noise,
-            radius,
-            height,
-            porosity,
-            drag_coefficient,
-        )
-        self.parachutes.append(parachute)
-        return self.parachutes[-1]
+        if parachute is not None:
+            if not isinstance(parachute, Parachute):
+                raise TypeError(
+                    "The 'parachute' argument must be an instance of a Parachute "
+                    "subclass (e.g. 'HemisphericalParachute')."
+                )
+            self.parachutes.append(parachute)
+        else:
+            # For backwards compatibility
+            deprecation_message = (
+                "Passing parachute parameters directly to 'add_parachute' method is "
+                + "deprecated and will be removed in version 1.14.0. Please create "
+                + "an object of class 'HemisphericalParachute' and pass it to the "
+                + "'parachute' argument of 'add_parachute' for the same behavior."
+            )
+            warn(message=deprecation_message, category=FutureWarning, stacklevel=2)
+            if name is None:
+                raise ValueError("Invalid 'name' argument! Please provide a string!")
+            if cd_s is None:
+                raise ValueError("Invalid 'cd_s' argument! Please provide a float!")
+            if trigger is None:
+                raise ValueError(
+                    "Invalid 'trigger' argument! Please provide a callable, float, or string!"
+                )
+            legacy_parachute = HemisphericalParachute(
+                name,
+                cd_s,
+                trigger,
+                sampling_rate,
+                lag,
+                noise,
+                radius,
+                height,
+                porosity,
+                drag_coefficient,
+            )
+            self.parachutes.append(legacy_parachute)
+            return self.parachutes[-1]
 
     def add_sensor(self, sensor, position):
         """Adds a sensor to the rocket.
@@ -1630,8 +1795,7 @@ def add_sensor(self, sensor, position):
             must be in the format (x, y, z) where x, y, and z are defined in the
             rocket's user defined coordinate system. If a single value is
             passed, it is assumed to be along the z-axis (centerline) of the
-            rocket's user defined coordinate system and angular_position and
-            radius must be given.
+            rocket's user defined coordinate system.
 
         Returns
         -------
@@ -1697,15 +1861,19 @@ def add_air_brakes(
             This function is expected to take the following arguments, in order:
 
             1. `time` (float): The current simulation time in seconds.
-            2. `sampling_rate` (float): The rate at which the controller
-               function is called, measured in Hertz (Hz).
+            2. `sampling_rate` (float or None): The rate at which the controller
+               function is called, measured in Hertz (Hz). It is None for
+               continuous controllers (called every solver step), so any
+               `1 / sampling_rate` computation must guard against None.
             3. `state` (list): The state vector of the simulation, structured as
                `[x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]`.
             4. `state_history` (list): A record of the rocket's state at each
-               step throughout the simulation. The state_history is organized as a
-               list of lists, with each sublist containing a state vector. The last
-               item in the list always corresponds to the previous state vector,
-               providing a chronological sequence of the rocket's evolving states.
+               step throughout the simulation. It is organized as a list of
+               lists, ordered oldest to newest, where each sublist is a
+               *time-prefixed* state row `[t, x, y, z, vx, vy, vz, e0, e1, e2,
+               e3, wx, wy, wz]` (the same layout as `Flight.solution`, one
+               leading `time` element ahead of the `state` layout in item 3).
+               The last item corresponds to the most recent recorded step.
             5. `observed_variables` (list): A list containing the variables that
                the controller function returns. The initial value in the first
                step of the simulation of this list is provided by the
@@ -1825,7 +1993,7 @@ def set_rail_buttons(
             as the rotation around the symmetry axis of the rocket
             relative to one of the other principal axis.
             Default value is 45 degrees, generally used in rockets with
-            4 fins.
+            4 fins. See :ref:`Angular Position Inputs <angular_position>`
         radius : int, float, optional
             Fuselage radius where the rail buttons are located.
 
diff --git a/rocketpy/sensitivity/sensitivity_model.py b/rocketpy/sensitivity/sensitivity_model.py
index 428897bff..737a46097 100644
--- a/rocketpy/sensitivity/sensitivity_model.py
+++ b/rocketpy/sensitivity/sensitivity_model.py
@@ -1,9 +1,13 @@
+import logging
+
 import numpy as np
 
 from rocketpy.plots.sensitivity_plots import _SensitivityModelPlots
 from rocketpy.prints.sensitivity_prints import _SensitivityModelPrints
 from rocketpy.tools import check_requirement_version, import_optional_dependency
 
+logger = logging.getLogger(__name__)
+
 
 class SensitivityModel:
     """Performs a 'local variance based first-order
@@ -354,11 +358,13 @@ def __check_requirements(self):
                 check_requirement_version(module_name, version)
             except (ValueError, ImportError) as e:  # pragma: no cover
                 has_error = True
-                print(
-                    f"The following error occurred while importing {module_name}: {e}"
+                logger.error(
+                    "The following error occurred while importing %s: %s",
+                    module_name,
+                    e,
                 )
         if has_error:  # pragma: no cover
-            print(
+            logger.error(
                 "Given the above errors, some methods may not work. Please run "
-                + "'pip install rocketpy[sensitivity]' to install extra requirements."
+                "'pip install rocketpy[sensitivity]' to install extra requirements."
             )
diff --git a/rocketpy/sensors/sensor.py b/rocketpy/sensors/sensor.py
index 0b44aeb18..137505272 100644
--- a/rocketpy/sensors/sensor.py
+++ b/rocketpy/sensors/sensor.py
@@ -1,4 +1,5 @@
 import json
+import logging
 import warnings
 from abc import ABC, abstractmethod
 
@@ -6,6 +7,8 @@
 
 from rocketpy.mathutils.vector_matrix import Matrix, Vector
 
+logger = logging.getLogger(__name__)
+
 
 # pylint: disable=too-many-statements
 class Sensor(ABC):
@@ -235,24 +238,25 @@ def _generic_export_measured_data(self, filename, file_format, data_labels):
         if file_format.lower() == "csv":
             # if sensor has been added multiple times to the simulated rocket
             if isinstance(self.measured_data[0], list):
-                print("Data saved to", end=" ")
+                saved = []
                 for i, data in enumerate(self.measured_data):
                     with open(filename + f"_{i + 1}", "w") as f:
                         f.write(",".join(data_labels) + "\n")
                         for entry in data:
                             f.write(",".join(map(str, entry)) + "\n")
-                    print(filename + f"_{i + 1},", end=" ")
+                    saved.append(filename + f"_{i + 1}")
+                logger.info("Data saved to: %s", ", ".join(saved))
             else:
                 with open(filename, "w") as f:
                     f.write(",".join(data_labels) + "\n")
                     for entry in self.measured_data:
                         f.write(",".join(map(str, entry)) + "\n")
-                print(f"Data saved to {filename}")
+                logger.info("Data saved to %s", filename)
             return
 
         if file_format.lower() == "json":
             if isinstance(self.measured_data[0], list):
-                print("Data saved to", end=" ")
+                saved = []
                 for i, data in enumerate(self.measured_data):
                     data_dict = {label: [] for label in data_labels}
                     for entry in data:
@@ -260,7 +264,8 @@ def _generic_export_measured_data(self, filename, file_format, data_labels):
                             data_dict[label].append(value)
                     with open(filename + f"_{i + 1}", "w") as f:
                         json.dump(data_dict, f)
-                    print(filename + f"_{i + 1},", end=" ")
+                    saved.append(filename + f"_{i + 1}")
+                logger.info("Data saved to: %s", ", ".join(saved))
             else:
                 data_dict = {label: [] for label in data_labels}
                 for entry in self.measured_data:
@@ -268,7 +273,7 @@ def _generic_export_measured_data(self, filename, file_format, data_labels):
                         data_dict[label].append(value)
                 with open(filename, "w") as f:
                     json.dump(data_dict, f)
-                print(f"Data saved to {filename}")
+                logger.info("Data saved to %s", filename)
             return
 
     # pylint: disable=unused-argument
diff --git a/rocketpy/simulation/flight.py b/rocketpy/simulation/flight.py
index 1443d1d80..cda75766b 100644
--- a/rocketpy/simulation/flight.py
+++ b/rocketpy/simulation/flight.py
@@ -1,4 +1,5 @@
 # pylint: disable=too-many-lines
+import logging
 import math
 import warnings
 from copy import deepcopy
@@ -7,8 +8,6 @@
 import numpy as np
 from scipy.integrate import BDF, DOP853, LSODA, RK23, RK45, OdeSolver, Radau
 
-from rocketpy.simulation.flight_data_exporter import FlightDataExporter
-
 from ..mathutils.function import Function, funcify_method
 from ..mathutils.vector_matrix import Matrix, Vector
 from ..motors.point_mass_motor import PointMassMotor
@@ -27,6 +26,8 @@
     quaternions_to_spin,
 )
 
+logger = logging.getLogger(__name__)
+
 ODE_SOLVER_MAP = {
     "RK23": RK23,
     "RK45": RK45,
@@ -196,6 +197,10 @@ class Flight:
         impacts the ground.
     Flight.parachute_events : array
         List that stores parachute events triggered during flight.
+    Flight.parachutes_info : dict
+        A dictionary whose keys are the parachute names and values
+        are the relevant dynamic variables calculated by that
+        parachute model.
     Flight.function_evaluations : array
         List that stores number of derivative function evaluations
         during numerical integration in cumulative manner.
@@ -587,6 +592,9 @@ def __init__(  # pylint: disable=too-many-arguments,too-many-statements
             A custom ``scipy.integrate.OdeSolver`` can be passed as well.
             For more information on the integration methods, see the scipy
             documentation [1]_.
+        simulation_mode : str, optional
+            Simulation mode to use. Can be "6 DOF" for 6 degrees of freedom or
+            "3 DOF" for 3 degrees of freedom. Default is "6 DOF".
         Returns
         -------
         None
@@ -598,6 +606,11 @@ def __init__(  # pylint: disable=too-many-arguments,too-many-statements
         # Save arguments
         self.env = environment
         self.rocket = rocket
+        # Warn about an aerodynamically unstable rocket now that it is fully
+        # assembled and about to be simulated. Doing it here (instead of on every
+        # add_surfaces call during construction) avoids spurious warnings for
+        # partially-built rockets that are ultimately stable.
+        self.rocket.warn_if_unstable()
         self.rail_length = rail_length
         if self.rail_length <= 0:  # pragma: no cover
             raise ValueError("Rail length must be a positive value.")
@@ -698,15 +711,6 @@ def __simulate(self, verbose):
 
                 self.__process_sensors_and_controllers_at_current_node(node, phase)
 
-                for controller in node._controllers:
-                    controller(
-                        self.t,
-                        self.y_sol,
-                        self.solution,
-                        self.sensors,
-                        self.env,
-                    )
-
                 for parachute in node.parachutes:
                     # Calculate and save pressure signal
                     (
@@ -715,11 +719,14 @@ def __simulate(self, verbose):
                     ) = self.__calculate_and_save_pressure_signals(
                         parachute, node.t, self.y_sol[2]
                     )
-                    if parachute.triggerfunc(
+                    if self._evaluate_parachute_trigger(
+                        parachute,
                         noisy_pressure,
                         height_above_ground_level,
                         self.y_sol,
                         self.sensors,
+                        phase.derivative,
+                        self.t,
                     ):
                         # Remove parachute from flight parachutes
                         self.parachutes.remove(parachute)
@@ -735,30 +742,11 @@ def __simulate(self, verbose):
                             )
                             i += 1
                         # Create flight phase for time after inflation
-                        callbacks = [
-                            lambda self, parachute_cd_s=parachute.cd_s: setattr(
-                                self, "parachute_cd_s", parachute_cd_s
-                            ),
-                            lambda self, parachute_radius=parachute.radius: setattr(
-                                self, "parachute_radius", parachute_radius
-                            ),
-                            lambda self, parachute_height=parachute.height: setattr(
-                                self, "parachute_height", parachute_height
-                            ),
-                            lambda self, parachute_porosity=parachute.porosity: setattr(
-                                self, "parachute_porosity", parachute_porosity
-                            ),
-                            lambda self, added_mass_coefficient=parachute.added_mass_coefficient: (
-                                setattr(
-                                    self,
-                                    "parachute_added_mass_coefficient",
-                                    added_mass_coefficient,
-                                )
-                            ),
-                        ]
+                        callbacks = []
+                        u_dot_parachute = self.u_dot_parachute_wrapper(parachute)
                         self.flight_phases.add_phase(
                             node.t + parachute.lag,
-                            self.u_dot_parachute,
+                            u_dot_parachute,
                             callbacks,
                             clear=False,
                             index=phase_index + i,
@@ -786,7 +774,16 @@ def __simulate(self, verbose):
                     self.y_sol = phase.solver.y
                     if verbose:
                         print(f"Current Simulation Time: {self.t:3.4f} s", end="\r")
-
+                        logger.debug("Current Simulation Time: %3.4f s", self.t)
+
+                    for controller in self._continuous_controllers:
+                        controller(
+                            self.t,
+                            self.y_sol,
+                            self.solution,
+                            self.sensors,
+                            self.env,
+                        )
                     if self.__check_simulation_events(phase, phase_index, node_index):
                         break  # Stop if simulation termination event occurred
 
@@ -810,6 +807,7 @@ def __simulate(self, verbose):
             self.__cache_sensor_data()
         if verbose:
             print(f"\n>>> Simulation Completed at Time: {self.t:3.4f} s")
+        logger.info("Simulation completed at time: %3.4f s", self.t)
 
     def __setup_phase_time_nodes(self, phase):
         """Set up time nodes for the current phase.
@@ -853,7 +851,7 @@ def __process_sensors_and_controllers_at_current_node(self, node, phase):
         phase : FlightPhase
             The current flight phase.
         """
-        if self.sensors:
+        if node._component_sensors:
             u_dot = phase.derivative(self.t, self.y_sol)
             self.__measure_sensors(node._component_sensors, u_dot)
 
@@ -932,11 +930,14 @@ def __check_and_handle_parachute_triggers(
             ) = self.__calculate_and_save_pressure_signals(
                 parachute, node.t, self.y_sol[2]
             )
-            if not parachute.triggerfunc(
+            if not self._evaluate_parachute_trigger(
+                parachute,
                 noisy_pressure,
                 height_above_ground_level,
                 self.y_sol,
                 self.sensors,
+                phase.derivative,
+                node.t,
             ):
                 continue  # Check next parachute
 
@@ -959,30 +960,10 @@ def __check_and_handle_parachute_triggers(
                 i += 1
 
             # Create flight phase for time after inflation
-            callbacks = [
-                lambda self, parachute_cd_s=parachute.cd_s: setattr(
-                    self, "parachute_cd_s", parachute_cd_s
-                ),
-                lambda self, parachute_radius=parachute.radius: setattr(
-                    self, "parachute_radius", parachute_radius
-                ),
-                lambda self, parachute_height=parachute.height: setattr(
-                    self, "parachute_height", parachute_height
-                ),
-                lambda self, parachute_porosity=parachute.porosity: setattr(
-                    self, "parachute_porosity", parachute_porosity
-                ),
-                lambda self, added_mass_coefficient=parachute.added_mass_coefficient: (
-                    setattr(
-                        self,
-                        "parachute_added_mass_coefficient",
-                        added_mass_coefficient,
-                    )
-                ),
-            ]
+            callbacks = []
             self.flight_phases.add_phase(
                 node.t + parachute.lag,
-                self.u_dot_parachute,
+                self.u_dot_parachute_wrapper(parachute),
                 callbacks,
                 clear=False,
                 index=phase_index + i,
@@ -1343,11 +1324,14 @@ def __check_overshootable_parachute_triggers(
             )
 
             # Check for parachute trigger
-            if not parachute.triggerfunc(
+            if not self._evaluate_parachute_trigger(
+                parachute,
                 noisy_pressure,
                 height_above_ground_level,
                 overshootable_node.y_sol,
                 self.sensors,
+                phase.derivative,
+                overshootable_node.t,
             ):
                 continue  # Check next parachute
 
@@ -1367,30 +1351,10 @@ def __check_overshootable_parachute_triggers(
                 i += 1
 
             # Create flight phase for time after inflation
-            callbacks = [
-                lambda self, parachute_cd_s=parachute.cd_s: setattr(
-                    self, "parachute_cd_s", parachute_cd_s
-                ),
-                lambda self, parachute_radius=parachute.radius: setattr(
-                    self, "parachute_radius", parachute_radius
-                ),
-                lambda self, parachute_height=parachute.height: setattr(
-                    self, "parachute_height", parachute_height
-                ),
-                lambda self, parachute_porosity=parachute.porosity: setattr(
-                    self, "parachute_porosity", parachute_porosity
-                ),
-                lambda self, added_mass_coefficient=parachute.added_mass_coefficient: (
-                    setattr(
-                        self,
-                        "parachute_added_mass_coefficient",
-                        added_mass_coefficient,
-                    )
-                ),
-            ]
+            callbacks = []
             self.flight_phases.add_phase(
                 overshootable_node.t + parachute.lag,
-                self.u_dot_parachute,
+                self.u_dot_parachute_wrapper(parachute),
                 callbacks,
                 clear=False,
                 index=phase_index + i,
@@ -1448,6 +1412,51 @@ def __calculate_and_save_pressure_signals(self, parachute, t, z):
 
         return noisy_pressure, height_above_ground_level
 
+    def _evaluate_parachute_trigger(
+        self, parachute, pressure, height, y, sensors, derivative_func, t
+    ):
+        """Evaluate parachute trigger, passing both sensors and u_dot to wrapper.
+
+        This helper preserves backward compatibility with existing trigger
+        signatures. The wrapper in Parachute always expects (p, h, y, sensors, u_dot)
+        and Flight computes u_dot only when the trigger requests it (optimization).
+
+        Parameters
+        ----------
+        parachute : Parachute
+            Parachute object.
+        pressure : float
+            Noisy pressure value passed to trigger.
+        height : float
+            Height above ground level passed to trigger.
+        y : array
+            State vector at evaluation time.
+        sensors : list
+            Sensors list passed to trigger.
+        derivative_func : callable
+            Function to compute derivatives: derivative_func(t, y)
+        t : float
+            Time at which to evaluate derivatives.
+
+        Returns
+        -------
+        bool
+            True if trigger condition met, False otherwise.
+        """
+        triggerfunc = parachute.triggerfunc
+
+        # Check wrapper metadata for expectations
+        expects_udot = getattr(triggerfunc, "_expects_udot", False)
+
+        # Compute u_dot only if needed (performance optimization)
+        u_dot = None
+        if expects_udot:
+            u_dot = derivative_func(t, y)
+
+        # Call the wrapper with both sensors and u_dot
+        # The wrapper will decide which args to pass to the user's function
+        return triggerfunc(pressure, height, y, sensors, u_dot)
+
     def __init_solution_monitors(self):
         # Initialize solution monitors
         self.out_of_rail_time = 0
@@ -1461,6 +1470,7 @@ def __init_solution_monitors(self):
         self.impact_velocity = 0
         self.impact_state = np.array([0])
         self.parachute_events = []
+        self.parachutes_info = {}
         self.__post_processed_variables = []
 
     def __init_flight_state(self):
@@ -1585,6 +1595,7 @@ def __init_equations_of_motion(self):
     def __init_controllers(self):
         """Initialize controllers and sensors"""
         self._controllers = self.rocket._controllers[:]
+        self._continuous_controllers = [c for c in self._controllers if c.is_continuous]
         self.sensors = self.rocket.sensors.get_components()
 
         # reset controllable object to initial state (only airbrakes for now)
@@ -2624,87 +2635,55 @@ def u_dot_generalized(self, t, u, post_processing=False):  # pylint: disable=too
 
         return u_dot
 
-    def u_dot_parachute(self, t, u, post_processing=False):
-        """Calculates derivative of u state vector with respect to time
-        when rocket is flying under parachute. A 3 DOF approximation is
-        used.
+    def u_dot_parachute_wrapper(self, parachute):
+        """Creates a wrapper for the u_dot_parachute used to solve the equations of
+        motion when that parachute is triggered. The reason is the following:
+        each parachute implements its own u_dot. This u_dot takes as argument the
+        state variable 'u', the time 't', and additional flight information as
+        'flight_information'. However, the solver (which is in the Flight class)
+        only allows u_dot to take 'u' and 't' as arguments. Hence, this wrapper
+        wraps the output of the u_dot to match the expected arguments of the
+        solver.
 
         Parameters
         ----------
-        t : float
-            Time in seconds
-        u : list
-            State vector defined by u = [x, y, z, vx, vy, vz, e0, e1,
-            e2, e3, omega1, omega2, omega3].
-        post_processing : bool, optional
-            If True, adds flight data information directly to self
-            variables such as self.angle_of_attack. Default is False.
+        parachute : Parachute
+            Parachute that is current executing the equations of motion
 
         Return
         ------
-        u_dot : list
-            State vector defined by u_dot = [vx, vy, vz, ax, ay, az,
-            e0dot, e1dot, e2dot, e3dot, alpha1, alpha2, alpha3].
+        u_dot_parachute : function
+            A augmented (with flight information) u_dot_parachute used in the solver
 
         """
-        # Get relevant state data
-        z, vx, vy, vz = u[2:6]
-
-        # Get atmospheric data
-        rho = self.env.density.get_value_opt(z)
-        wind_velocity_x = self.env.wind_velocity_x.get_value_opt(z)
-        wind_velocity_y = self.env.wind_velocity_y.get_value_opt(z)
-
-        # Get the mass of the rocket
-        mp = self.rocket.dry_mass
-
-        # to = 1.2
-        # eta = 1
-        # Rdot = (6 * R * (1 - eta) / (1.2**6)) * (
-        #     (1 - eta) * t**5 + eta * (to**3) * (t**2)
-        # )
-        # Rdot = 0
-
-        # tf = 8 * nominal diameter / velocity at line stretch
-
-        # Calculate added mass
-        ma = (
-            self.parachute_added_mass_coefficient
-            * rho
-            * (2 / 3)
-            * np.pi
-            * self.parachute_radius**2
-            * self.parachute_height
-        )
-
-        # Calculate freestream speed
-        freestream_x = vx - wind_velocity_x
-        freestream_y = vy - wind_velocity_y
-        freestream_z = vz
-        free_stream_speed = (freestream_x**2 + freestream_y**2 + freestream_z**2) ** 0.5
-
-        # Determine drag force
-        pseudo_drag = -0.5 * rho * self.parachute_cd_s * free_stream_speed
-        # pseudo_drag = pseudo_drag - ka * rho * 4 * np.pi * (R**2) * Rdot
-        Dx = pseudo_drag * freestream_x  # add eta efficiency for wake
-        Dy = pseudo_drag * freestream_y
-        Dz = pseudo_drag * freestream_z
-        ax = Dx / (mp + ma)
-        ay = Dy / (mp + ma)
-        az = (Dz - mp * self.env.gravity.get_value_opt(z)) / (mp + ma)
-
-        # Add coriolis acceleration
-        _, w_earth_y, w_earth_z = self.env.earth_rotation_vector
-        ax -= 2 * (vz * w_earth_y - vy * w_earth_z)
-        ay -= 2 * (vx * w_earth_z)
-        az -= 2 * (-vx * w_earth_y)
+        # additional information used for the u_dot_parachute equations
+        flight_information = {
+            "env": self.env,
+            "rocket": self.rocket,
+        }
 
-        if post_processing:
-            self.__post_processed_variables.append(
-                [t, ax, ay, az, 0, 0, 0, Dx, Dy, Dz, 0, 0, 0, 0]
+        def u_dot_parachute(t, u, post_processing=False):
+            parachute_output = parachute.u_dot(
+                t=t,
+                u=u,
+                flight_information=flight_information,
+                post_processing=post_processing,
             )
+            state = parachute_output["state"]
+            if post_processing:
+                # The parachute dynamic information (e.g. drag) must be saved
+                # over the accepted solution steps, which are only replayed
+                # during post-processing. Saving it during the raw integration
+                # would also store the solver's internal and rejected steps,
+                # polluting the ``parachutes_info`` time series.
+                post_processing_info = parachute_output["post_processing_information"]
+                self.__post_processed_variables.append(post_processing_info)
+                parachute.add_information_to_flight(
+                    self, parachute_output["additional_info"]
+                )
+            return state
 
-        return [vx, vy, vz, ax, ay, az, 0, 0, 0, 0, 0, 0, 0]
+        return u_dot_parachute
 
     @cached_property
     def solution_array(self):
@@ -3994,10 +3973,17 @@ def __transform_pressure_signals_lists_to_functions(self):
             parachute.noise_signal_function = Function(
                 parachute.noise_signal, "Time (s)", "Pressure Noise (Pa)", "linear"
             )
+            # Function arithmetic drops the axis labels/title, so restore them
+            # to keep the pressure-signal plots readable (see pressure_signals).
             parachute.noisy_pressure_signal_function = (
                 parachute.clean_pressure_signal_function
                 + parachute.noise_signal_function
             )
+            parachute.noisy_pressure_signal_function.set_inputs("Time (s)")
+            parachute.noisy_pressure_signal_function.set_outputs(
+                "Pressure - With Noise (Pa)"
+            )
+            parachute.noisy_pressure_signal_function.set_title("Noisy Pressure Signal")
 
     @cached_property
     def __evaluate_post_process(self):
@@ -4026,11 +4012,20 @@ def __evaluate_post_process(self):
 
         return np.array(self.__post_processed_variables)
 
-    def calculate_stall_wind_velocity(self, stall_angle):  # TODO: move to utilities
-        """Function to calculate the maximum wind velocity before the angle of
-        attack exceeds a desired angle, at the instant of departing rail launch.
-        Can be helpful if you know the exact stall angle of all aerodynamics
-        surfaces.
+    @deprecated(
+        reason="This method is deprecated in version 1.13.0 and will be fully "
+        "removed by version 1.15.0",
+        alternative="rocketpy.utilities.calculate_stall_wind_velocity",
+    )
+    def calculate_stall_wind_velocity(self, stall_angle):
+        """Calculate the maximum wind velocity before the angle of attack exceeds
+        a desired angle, at the instant of departing rail launch. Can be helpful
+        if you know the exact stall angle of all aerodynamics surfaces.
+
+        .. deprecated:: 1.13.0
+           This method is deprecated and will be fully removed by version
+           1.15.0. Use :func:`rocketpy.utilities.calculate_stall_wind_velocity`
+           instead.
 
         Parameters
         ----------
@@ -4040,97 +4035,23 @@ def calculate_stall_wind_velocity(self, stall_angle):  # TODO: move to utilities
 
         Return
         ------
-        None
-        """
-        v_f = self.out_of_rail_velocity
-
-        theta = np.radians(self.inclination)
-        stall_angle = np.radians(stall_angle)
-
-        c = (math.cos(stall_angle) ** 2 - math.cos(theta) ** 2) / math.sin(
-            stall_angle
-        ) ** 2
-        w_v = (
-            2 * v_f * math.cos(theta) / c
-            + (
-                4 * v_f * v_f * math.cos(theta) * math.cos(theta) / (c**2)
-                + 4 * 1 * v_f * v_f / c
-            )
-            ** 0.5
-        ) / 2
-
-        stall_angle = np.degrees(stall_angle)
-        print(
-            "Maximum wind velocity at Rail Departure time before angle"
-            + f" of attack exceeds {stall_angle:.3f}°: {w_v:.3f} m/s"
-        )
-
-    @deprecated(
-        reason="Moved to FlightDataExporter.export_pressures()",
-        version="v1.12.0",
-        alternative="rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_pressures",
-    )
-    def export_pressures(self, file_name, time_step):
-        """
-        .. deprecated:: 1.11
-           Use :class:`rocketpy.simulation.flight_data_exporter.FlightDataExporter`
-           and call ``.export_pressures(...)``.
-        """
-        return FlightDataExporter(self).export_pressures(file_name, time_step)
-
-    @deprecated(
-        reason="Moved to FlightDataExporter.export_data()",
-        version="v1.12.0",
-        alternative="rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_data",
-    )
-    def export_data(self, file_name, *variables, time_step=None):
-        """
-        .. deprecated:: 1.11
-           Use :class:`rocketpy.simulation.flight_data_exporter.FlightDataExporter`
-           and call ``.export_data(...)``.
+        float
+            Maximum wind velocity, in m/s, at rail departure before the angle of
+            attack exceeds ``stall_angle``.
         """
-        return FlightDataExporter(self).export_data(
-            file_name, *variables, time_step=time_step
+        # Imported lazily to avoid a circular import (utilities imports Flight).
+        from rocketpy.utilities import (  # pylint: disable=import-outside-toplevel
+            calculate_stall_wind_velocity,
         )
 
-    @deprecated(
-        reason="Moved to FlightDataExporter.export_sensor_data()",
-        version="v1.12.0",
-        alternative="rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_sensor_data",
-    )
-    def export_sensor_data(self, file_name, sensor=None):
-        """
-        .. deprecated:: 1.11
-           Use :class:`rocketpy.simulation.flight_data_exporter.FlightDataExporter`
-           and call ``.export_sensor_data(...)``.
-        """
-        return FlightDataExporter(self).export_sensor_data(file_name, sensor=sensor)
-
-    @deprecated(
-        reason="Moved to FlightDataExporter.export_kml()",
-        version="v1.12.0",
-        alternative="rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_kml",
-    )
-    def export_kml(
-        self,
-        file_name="trajectory.kml",
-        time_step=None,
-        extrude=True,
-        color="641400F0",
-        altitude_mode="absolute",
-    ):
-        """
-        .. deprecated:: 1.11
-           Use :class:`rocketpy.simulation.flight_data_exporter.FlightDataExporter`
-           and call ``.export_kml(...)``.
-        """
-        return FlightDataExporter(self).export_kml(
-            file_name=file_name,
-            time_step=time_step,
-            extrude=extrude,
-            color=color,
-            altitude_mode=altitude_mode,
+        w_v = calculate_stall_wind_velocity(self, stall_angle)
+        # Display for interactive use, but also return the value so it is never
+        # silently lost (it was previously only logged at INFO level).
+        print(
+            "Maximum wind velocity at Rail Departure time before angle "
+            f"of attack exceeds {stall_angle:.3f}°: {w_v:.3f} m/s"
         )
+        return w_v
 
     def info(self):
         """Prints out a summary of the data available about the Flight."""
@@ -4148,6 +4069,14 @@ def time_iterator(self, node_list):
             i += 1
 
     def to_dict(self, **kwargs):
+        # ``parachutes_info`` is populated as a side effect of the lazy
+        # post-processing pass (``add_information_to_flight`` is only called with
+        # ``post_processing=True``). Trigger that pass before reading the
+        # attribute so the per-parachute drag time series is serialized even for
+        # flights that have not been post-processed yet (e.g. flights without
+        # controllers that are saved before any acceleration/force property or
+        # plot is accessed). This is a no-op once post-processing has run.
+        _ = self.ax
         data = {
             "rocket": self.rocket,
             "env": self.env,
@@ -4171,6 +4100,7 @@ def to_dict(self, **kwargs):
             "apogee_time": self.apogee_time,
             "apogee": self.apogee,
             "parachute_events": self.parachute_events,
+            "parachutes_info": self.parachutes_info,
             "impact_state": self.impact_state,
             "impact_velocity": self.impact_velocity,
             "x_impact": self.x_impact,
@@ -4276,8 +4206,8 @@ def __repr__(self):
             return str(self.list)
 
         def display_warning(self, *messages):  # pragma: no cover
-            """A simple function to print a warning message."""
-            print("WARNING:", *messages)
+            """A simple function to log a warning message."""
+            logger.warning(" ".join(str(m) for m in messages))
 
         def add(self, flight_phase, index=None):  # TODO: quite complex method
             """Add a flight phase to the list. It will be inserted in the
@@ -4497,6 +4427,9 @@ def add_parachutes(self, parachutes, t_init, t_end):
 
         def add_controllers(self, controllers, t_init, t_end):
             for controller in controllers:
+                # Skip node creation for continuous controllers
+                if controller.is_continuous:
+                    continue
                 # Calculate start of sampling time nodes
                 controller_time_step = 1 / controller.sampling_rate
                 controller_node_list = [
diff --git a/rocketpy/simulation/flight_comparator.py b/rocketpy/simulation/flight_comparator.py
index 7f1b34286..19785000a 100644
--- a/rocketpy/simulation/flight_comparator.py
+++ b/rocketpy/simulation/flight_comparator.py
@@ -396,7 +396,6 @@ def _plot_external_sources(
                 (rmse / mean_abs_y_sim) * 100 if mean_abs_y_sim != 0 else np.inf
             )
 
-            # Print Metrics
             print(f"Source: {label}")
             print(f"  - MAE:            {mae:.4f}")
             print(f"  - RMSE:           {rmse:.4f}")
diff --git a/rocketpy/simulation/flight_data_exporter.py b/rocketpy/simulation/flight_data_exporter.py
index 8bdc53c17..80ee051c7 100644
--- a/rocketpy/simulation/flight_data_exporter.py
+++ b/rocketpy/simulation/flight_data_exporter.py
@@ -3,10 +3,13 @@
 """
 
 import json
+import logging
 
 import numpy as np
 import simplekml
 
+logger = logging.getLogger(__name__)
+
 
 class FlightDataExporter:
     """Export data from a rocketpy.Flight object to various formats."""
@@ -57,7 +60,7 @@ def export_pressures(self, file_name, time_step):
         # pylint: disable=W1514, E1121
         with open(file_name, "w") as file:
             if len(f.rocket.parachutes) == 0:
-                print("No parachutes in the rocket, saving static pressure.")
+                logger.info("No parachutes in the rocket, saving static pressure.")
                 for t in time_points:
                     file.write(f"{t:f}, {f.pressure.get_value_opt(t):.5f}\n")
             else:
@@ -210,7 +213,7 @@ def export_sensor_data(self, file_name, sensor=None):
 
         with open(file_name, "w") as file:
             json.dump(data_dict, file)
-        print("Sensor data exported to: ", file_name)
+        logger.info("Sensor data exported to: %s", file_name)
 
     def export_kml(
         self,
@@ -295,4 +298,4 @@ def export_kml(
 
         # Save the KML
         kml.save(file_name)
-        print("File ", file_name, " saved with success!")
+        logger.info("File %s saved with success!", file_name)
diff --git a/rocketpy/simulation/flight_data_importer.py b/rocketpy/simulation/flight_data_importer.py
index b4498a1dc..cec357fd5 100644
--- a/rocketpy/simulation/flight_data_importer.py
+++ b/rocketpy/simulation/flight_data_importer.py
@@ -2,6 +2,7 @@
 and build a rocketpy.Flight object from it.
 """
 
+import logging
 from os import listdir
 from os.path import isfile, join
 
@@ -10,6 +11,8 @@
 from rocketpy.mathutils import Function
 from rocketpy.units import UNITS_CONVERSION_DICT
 
+logger = logging.getLogger(__name__)
+
 FLIGHT_LABEL_MAP = {
     # "name of Flight Attribute": "Label to be displayed"
     "acceleration": "Acceleration (m/s^2)",
@@ -285,7 +288,7 @@ def __create_attributes(self, filepath, interpolation, extrapolation):
             # Convert units if necessary
             if units and col in units:
                 values /= UNITS_CONVERSION_DICT[units[col]]
-                print(f"Attribute '{name}' converted from {units[col]} to SI")
+                logger.debug("Attribute '%s' converted from %s to SI", name, units[col])
 
             # Create Function object and set as attribute
             setattr(
@@ -301,9 +304,8 @@ def __create_attributes(self, filepath, interpolation, extrapolation):
             )
             created.append(name)
 
-        print(
-            "The following attributes were create and are now available to be used: ",
-            created,
+        logger.info(
+            "The following attributes were created and are now available: %s", created
         )
 
     def read_data(
diff --git a/rocketpy/simulation/monte_carlo.py b/rocketpy/simulation/monte_carlo.py
index e10789a7d..a7641595a 100644
--- a/rocketpy/simulation/monte_carlo.py
+++ b/rocketpy/simulation/monte_carlo.py
@@ -13,6 +13,7 @@
 latest documentation.
 """
 
+import csv
 import json
 import os
 import traceback
@@ -37,7 +38,7 @@
 # TODO: Create evolution plots to analyze convergence
 
 
-class MonteCarlo:
+class MonteCarlo:  # pylint: disable=too-many-public-methods
     """Class to run a Monte Carlo simulation of a rocket flight.
 
     Attributes
@@ -222,7 +223,7 @@ def simulate(
         self.number_of_simulations = number_of_simulations
         self._initial_sim_idx = self.num_of_loaded_sims if append else 0
 
-        _SimMonitor.reprint("Starting Monte Carlo analysis")
+        print("Starting Monte Carlo analysis")
 
         self.__setup_files(append)
 
@@ -298,12 +299,12 @@ def __run_in_serial(self):
             sim_monitor.print_final_status()
 
         except KeyboardInterrupt:
-            _SimMonitor.reprint("Keyboard Interrupt, files saved.")
+            print("Keyboard interrupt received. Files saved.")
             with open(self._error_file, "a", encoding="utf-8") as f:
                 f.write(inputs_json)
 
         except Exception as error:
-            _SimMonitor.reprint(f"Error on iteration {sim_monitor.count}: {error}")
+            print(f"Error on iteration {sim_monitor.count}: {error}")
             with open(self._error_file, "a", encoding="utf-8") as f:
                 f.write(inputs_json)
             raise error
@@ -324,7 +325,7 @@ def __run_in_parallel(self, n_workers=None):
         """
         n_workers = self.__validate_number_of_workers(n_workers)
 
-        _SimMonitor.reprint(f"Running Monte Carlo simulation with {n_workers} workers.")
+        print(f"Running Monte Carlo simulation with {n_workers} workers.")
 
         multiprocess, managers = _import_multiprocess()
 
@@ -417,8 +418,12 @@ def __sim_producer(self, seed, sim_monitor, mutex, error_event):  # pylint: disa
                 try:
                     mutex.acquire()
                     if error_event.is_set():
-                        sim_monitor.reprint(
-                            "Simulation Interrupt, files from simulation "
+                        # Runs in a worker process spawned via multiprocessing:
+                        # logging handlers configured in the main process are
+                        # not guaranteed to be inherited (e.g. Windows "spawn"),
+                        # so this must use print() to remain visible.
+                        _SimMonitor.reprint(
+                            f"Simulation interrupt. Files from simulation "
                             f"{sim_idx} saved."
                         )
                         with open(self.error_file, "a", encoding="utf-8") as f:
@@ -440,8 +445,11 @@ def __sim_producer(self, seed, sim_monitor, mutex, error_event):  # pylint: disa
             with open(self.error_file, "a", encoding="utf-8") as f:
                 f.write(inputs_json)
 
-            sim_monitor.reprint(f"Error on iteration {sim_idx}:")
-            sim_monitor.reprint(traceback.format_exc())
+            # See note above: must use print() to remain visible from a
+            # multiprocessing worker process.
+            _SimMonitor.reprint(
+                f"Error on iteration {sim_idx}:\n{traceback.format_exc()}"
+            )
             error_event.set()
             mutex.release()
 
@@ -525,6 +533,107 @@ def estimate_confidence_interval(
 
         return res.confidence_interval
 
+    def simulate_convergence(
+        self,
+        target_attribute="apogee_time",
+        target_confidence=0.95,
+        tolerance=0.5,
+        max_simulations=1000,
+        batch_size=50,
+        parallel=False,
+        n_workers=None,
+    ):
+        """Run Monte Carlo simulations in batches until the confidence interval
+        width converges within the specified tolerance or the maximum number of
+        simulations is reached.
+
+        Parameters
+        ----------
+        target_attribute : str
+            The target attribute to track its convergence (e.g., "apogee", "apogee_time", etc.).
+        target_confidence : float, optional
+            The confidence level for the interval (between 0 and 1). Default is 0.95.
+        tolerance : float, optional
+            The desired width of the confidence interval in seconds, meters, or other units. Default is 0.5.
+        max_simulations : int, optional
+            The maximum number of simulations to run to avoid infinite loops. Default is 1000.
+        batch_size : int, optional
+            The number of simulations to run in each batch. Default is 50.
+        parallel : bool, optional
+            Whether to run simulations in parallel. Default is False.
+        n_workers : int, optional
+            The number of worker processes to use if running in parallel. Default is None.
+
+        Returns
+        -------
+        confidence_interval_history : list of float
+            History of confidence interval widths, one value per batch of simulations.
+            The last element corresponds to the width when the simulation stopped for
+            either meeting the tolerance or reaching the maximum number of simulations.
+        """
+
+        # Validate inputs up-front. Without this, a non-positive batch_size makes
+        # the loop run zero new simulations every iteration and spin forever.
+        if not isinstance(batch_size, (int, np.integer)) or batch_size <= 0:
+            raise ValueError(
+                f"'batch_size' must be a positive integer, got {batch_size!r}."
+            )
+        if not isinstance(max_simulations, (int, np.integer)) or max_simulations <= 0:
+            raise ValueError(
+                f"'max_simulations' must be a positive integer, got "
+                f"{max_simulations!r}."
+            )
+        if not isinstance(tolerance, (int, float)) or tolerance <= 0:
+            raise ValueError(
+                f"'tolerance' must be a positive number, got {tolerance!r}."
+            )
+        if not 0 < target_confidence < 1:
+            raise ValueError(
+                "'target_confidence' must be between 0 and 1 (exclusive), got "
+                f"{target_confidence!r}."
+            )
+
+        self.import_outputs(self.filename.with_suffix(".outputs.txt"))
+        confidence_interval_history = []
+
+        while self.num_of_loaded_sims < max_simulations:
+            total_sims = min(self.num_of_loaded_sims + batch_size, max_simulations)
+
+            self.simulate(
+                number_of_simulations=total_sims,
+                append=True,
+                include_function_data=False,
+                parallel=parallel,
+                n_workers=n_workers,
+            )
+
+            self.import_outputs(self.filename.with_suffix(".outputs.txt"))
+
+            ci = self.estimate_confidence_interval(
+                attribute=target_attribute,
+                confidence_level=target_confidence,
+            )
+
+            width = float(ci.high - ci.low)
+            confidence_interval_history.append(width)
+
+            # A NaN width means the target attribute contains NaN values; the
+            # tolerance check would never pass, so the loop would run to
+            # max_simulations and silently return a NaN history. Stop and warn.
+            if np.isnan(width):
+                warnings.warn(
+                    f"The confidence interval width for '{target_attribute}' is "
+                    "NaN, likely because the attribute contains NaN values. "
+                    "Stopping convergence early; check the simulation outputs.",
+                    stacklevel=2,
+                )
+                break
+
+            if width <= tolerance:
+                break
+
+        return confidence_interval_history
+
     def __evaluate_flight_inputs(self, sim_idx):
         """Evaluates the inputs of a single flight simulation.
 
@@ -601,7 +710,7 @@ def __terminate_simulation(self):
         self.output_file = self._output_file
         self.error_file = self._error_file
 
-        _SimMonitor.reprint(f"Results saved to {self._output_file}")
+        print(f"Results saved to {self._output_file}")
 
     def __check_export_list(self, export_list):
         """
@@ -807,58 +916,232 @@ def error_file(self, value):
         self._error_file = value
         self.set_errors_log()
 
+    # File format helpers
+
+    @staticmethod
+    def _detect_file_format(filepath):
+        """Detect file format from the file extension.
+
+        Parameters
+        ----------
+        filepath : str or Path
+            Path to the file.
+
+        Returns
+        -------
+        str
+            One of ``"jsonl"``, ``"csv"``, or ``"json"``.
+
+        Raises
+        ------
+        ValueError
+            If the file extension is not supported.
+        """
+        suffix = Path(filepath).suffix.lower()
+        format_map = {".txt": "jsonl", ".csv": "csv", ".json": "json"}
+        if suffix not in format_map:
+            raise ValueError(
+                f"Unsupported file extension '{suffix}'. "
+                "Expected '.txt', '.csv', or '.json'."
+            )
+        return format_map[suffix]
+
+    @staticmethod
+    def _parse_csv_value(value):
+        """Parse a string value from a CSV cell into its appropriate type.
+
+        Parameters
+        ----------
+        value : str
+            The raw string value from the CSV cell.
+
+        Returns
+        -------
+        int, float, dict, list, or str
+            The parsed value in its appropriate Python type.
+        """
+        if value == "":
+            return value
+        # Try parsing JSON objects/arrays
+        if value.startswith(("{", "[")):
+            try:
+                return json.loads(value)
+            except (json.JSONDecodeError, ValueError):
+                pass
+        # Try numeric types
+        try:
+            int_val = int(value)
+            # Ensure the string was truly an integer (not "1.0")
+            if str(int_val) == value:
+                return int_val
+        except ValueError:
+            pass
+        try:
+            return float(value)
+        except ValueError:
+            pass
+        return value
+
+    def _read_log_file(self, filepath):
+        """Read a log file in any supported format and return a list of dicts.
+
+        Parameters
+        ----------
+        filepath : str or Path
+            Path to the log file. Format is detected from the extension.
+
+        Returns
+        -------
+        list of dict
+            A list of dictionaries, one per simulation record.
+        """
+        fmt = self._detect_file_format(filepath)
+        result = []
+        with open(filepath, mode="r", encoding="utf-8") as f:
+            if fmt == "jsonl":
+                for line in f:
+                    line = line.strip()
+                    if line:
+                        result.append(json.loads(line))
+            elif fmt == "json":
+                content = f.read().strip()
+                if content:
+                    result = json.loads(content)
+            elif fmt == "csv":
+                reader = csv.DictReader(f)
+                for row in reader:
+                    result.append({k: self._parse_csv_value(v) for k, v in row.items()})
+        return result
+
+    @staticmethod
+    def _write_log_to_csv(log_data, filepath, flatten=False):
+        """Write a list of dicts to a CSV file.
+
+        Parameters
+        ----------
+        log_data : list of dict
+            The data to write. Each dict is one row.
+        filepath : str or Path
+            Output file path.
+        flatten : bool, optional
+            If True, non-scalar columns (dicts, lists) are omitted.
+            If False (default), non-scalar values are serialized as JSON
+            strings in the CSV cells.
+
+        Raises
+        ------
+        ValueError
+            If ``log_data`` is empty.
+        """
+        if not log_data:
+            raise ValueError(
+                "No data to export. Run a simulation first or import existing data."
+            )
+        # Collect all keys preserving insertion order
+        all_keys = list(dict.fromkeys(k for row in log_data for k in row))
+
+        if flatten:
+            # Identify scalar-only keys
+            scalar_keys = []
+            for key in all_keys:
+                if all(not isinstance(row.get(key), (dict, list)) for row in log_data):
+                    scalar_keys.append(key)
+            fieldnames = scalar_keys
+        else:
+            fieldnames = all_keys
+
+        with open(filepath, mode="w", newline="", encoding="utf-8") as f:
+            writer = csv.DictWriter(f, fieldnames=fieldnames, extrasaction="ignore")
+            writer.writeheader()
+            for row in log_data:
+                csv_row = {}
+                for key in fieldnames:
+                    value = row.get(key, "")
+                    if isinstance(value, (dict, list)):
+                        csv_row[key] = json.dumps(value)
+                    else:
+                        csv_row[key] = value
+                writer.writerow(csv_row)
+
+    def _write_log_to_json(self, log_data, filepath):
+        """Write a list of dicts to a JSON file as a proper JSON array.
+
+        Parameters
+        ----------
+        log_data : list of dict
+            The data to write. Each dict becomes one element of the array.
+        filepath : str or Path
+            Output file path.
+
+        Raises
+        ------
+        ValueError
+            If ``log_data`` is empty.
+        """
+        if not log_data:
+            raise ValueError(
+                "No data to export. Run a simulation first or import existing data."
+            )
+        with open(filepath, mode="w", encoding="utf-8") as f:
+            json.dump(log_data, f, cls=RocketPyEncoder, indent=2)
+
     # Setters for post simulation attributes
 
     def set_inputs_log(self):
         """
         Sets inputs_log from a file into an attribute for easy access.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Returns
         -------
         None
         """
-        self.inputs_log = []
-        with open(self.input_file, mode="r", encoding="utf-8") as rows:
-            for line in rows:
-                self.inputs_log.append(json.loads(line))
+        self.inputs_log = self._read_log_file(self.input_file)
 
     def set_outputs_log(self):
         """
         Sets outputs_log from a file into an attribute for easy access.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Returns
         -------
         None
         """
-        self.outputs_log = []
-        with open(self.output_file, mode="r", encoding="utf-8") as rows:
-            for line in rows:
-                self.outputs_log.append(json.loads(line))
+        self.outputs_log = self._read_log_file(self.output_file)
 
     def set_errors_log(self):
         """
         Sets errors_log from a file into an attribute for easy access.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Returns
         -------
         None
         """
-        self.errors_log = []
-        with open(self.error_file, mode="r", encoding="utf-8") as errors:
-            for line in errors:
-                self.errors_log.append(json.loads(line))
+        self.errors_log = self._read_log_file(self.error_file)
 
     def set_num_of_loaded_sims(self):
         """
         Determines the number of simulations loaded from output_file being
-        currently used.
+        currently used. Supports .txt (JSONL), .csv, and .json formats.
 
         Returns
         -------
         None
         """
+        fmt = self._detect_file_format(self.output_file)
         with open(self.output_file, mode="r", encoding="utf-8") as outputs:
-            self.num_of_loaded_sims = sum(1 for _ in outputs)
+            if fmt == "jsonl":
+                self.num_of_loaded_sims = sum(1 for _ in outputs)
+            elif fmt == "csv":
+                # Subtract 1 for the header row
+                self.num_of_loaded_sims = max(0, sum(1 for _ in outputs) - 1)
+            elif fmt == "json":
+                content = outputs.read().strip()
+                if content:
+                    self.num_of_loaded_sims = len(json.loads(content))
+                else:
+                    self.num_of_loaded_sims = 0
 
     def set_results(self):
         """
@@ -915,13 +1198,15 @@ def set_processed_results(self):
 
     def import_outputs(self, filename=None):
         """
-        Import Monte Carlo results from .txt file and save it into a dictionary.
+        Import Monte Carlo results from a file and save it into a dictionary.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Parameters
         ----------
         filename : str, optional
             Name or directory path to the file to be imported. If none,
-            self.filename will be used.
+            self.filename will be used with the default .outputs.txt suffix.
+            Files with .csv or .json extensions are also accepted.
 
         Returns
         -------
@@ -929,7 +1214,7 @@ def import_outputs(self, filename=None):
 
         Notes
         -----
-        Notice that you can import the outputs, inputs, and errors from the a
+        Notice that you can import the outputs, inputs, and errors from a
         file without the need to run simulations. You can use previously saved
         files to process analyze the results or to continue a simulation.
         """
@@ -942,20 +1227,22 @@ def import_outputs(self, filename=None):
             with open(filepath, "w+", encoding="utf-8"):
                 self.output_file = filepath
 
-        _SimMonitor.reprint(
-            f"A total of {self.num_of_loaded_sims} simulations results were "
-            f"loaded from the following output file: {self.output_file}\n"
+        print(
+            f"A total of {self.num_of_loaded_sims} simulation results were "
+            f"loaded from: {self.output_file}"
         )
 
     def import_inputs(self, filename=None):
         """
-        Import Monte Carlo inputs from .txt file and save it into a dictionary.
+        Import Monte Carlo inputs from a file and save it into a dictionary.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Parameters
         ----------
         filename : str, optional
             Name or directory path to the file to be imported. If none,
-            self.filename will be used.
+            self.filename will be used with the default .inputs.txt suffix.
+            Files with .csv or .json extensions are also accepted.
 
         Returns
         -------
@@ -970,17 +1257,19 @@ def import_inputs(self, filename=None):
             with open(filepath, "w+", encoding="utf-8"):
                 self.input_file = filepath
 
-        _SimMonitor.reprint(f"The following input file was imported: {self.input_file}")
+        print(f"The following input file was imported: {self.input_file}")
 
     def import_errors(self, filename=None):
         """
-        Import Monte Carlo errors from .txt file and save it into a dictionary.
+        Import Monte Carlo errors from a file and save it into a dictionary.
+        Supports .txt (JSONL), .csv, and .json file formats.
 
         Parameters
         ----------
         filename : str, optional
             Name or directory path to the file to be imported. If none,
-            self.filename will be used.
+            self.filename will be used with the default .errors.txt suffix.
+            Files with .csv or .json extensions are also accepted.
 
         Returns
         -------
@@ -995,11 +1284,11 @@ def import_errors(self, filename=None):
             with open(filepath, "w+", encoding="utf-8"):
                 self.error_file = filepath
 
-        _SimMonitor.reprint(f"The following error file was imported: {self.error_file}")
+        print(f"The following error file was imported: {self.error_file}")
 
     def import_results(self, filename=None):
         """
-        Import Monte Carlo results from .txt file and save it into a dictionary.
+        Import Monte Carlo results from a file and save it into a dictionary.
 
         Parameters
         ----------
@@ -1214,6 +1503,109 @@ def compare_ellipses(self, other_monte_carlo, **kwargs):
         """
         self.plots.ellipses_comparison(other_monte_carlo, **kwargs)
 
+    # CSV and JSON export methods
+
+    def export_outputs_to_csv(self, filename):
+        """Export simulation outputs to a CSV file.
+
+        Each row represents one simulation. All output values are scalar,
+        so the CSV is directly usable in spreadsheet applications.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output CSV file.
+
+        Raises
+        ------
+        ValueError
+            If no output data is available to export.
+        """
+        self._write_log_to_csv(self.outputs_log, filename)
+
+    def export_outputs_to_json(self, filename):
+        """Export simulation outputs to a JSON file as an array of objects.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output JSON file.
+
+        Raises
+        ------
+        ValueError
+            If no output data is available to export.
+        """
+        self._write_log_to_json(self.outputs_log, filename)
+
+    def export_inputs_to_csv(self, filename, flatten=False):
+        """Export simulation inputs to a CSV file.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output CSV file.
+        flatten : bool, optional
+            If True, columns with non-scalar values (dicts, lists) are
+            omitted from the CSV. If False (default), non-scalar values
+            are serialized as JSON strings within the CSV cells.
+
+        Raises
+        ------
+        ValueError
+            If no input data is available to export.
+        """
+        self._write_log_to_csv(self.inputs_log, filename, flatten=flatten)
+
+    def export_inputs_to_json(self, filename):
+        """Export simulation inputs to a JSON file as an array of objects.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output JSON file.
+
+        Raises
+        ------
+        ValueError
+            If no input data is available to export.
+        """
+        self._write_log_to_json(self.inputs_log, filename)
+
+    def export_errors_to_csv(self, filename, flatten=False):
+        """Export simulation errors to a CSV file.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output CSV file.
+        flatten : bool, optional
+            If True, columns with non-scalar values (dicts, lists) are
+            omitted from the CSV. If False (default), non-scalar values
+            are serialized as JSON strings within the CSV cells.
+
+        Raises
+        ------
+        ValueError
+            If no error data is available to export.
+        """
+        self._write_log_to_csv(self.errors_log, filename, flatten=flatten)
+
+    def export_errors_to_json(self, filename):
+        """Export simulation errors to a JSON file as an array of objects.
+
+        Parameters
+        ----------
+        filename : str
+            Path to the output JSON file.
+
+        Raises
+        ------
+        ValueError
+            If no error data is available to export.
+        """
+        self._write_log_to_json(self.errors_log, filename)
+
 
 def _import_multiprocess():
     """Import the necessary modules and submodules for the
@@ -1308,15 +1700,12 @@ def print_final_status(self):
         msg = f"Completed {self.count - self.initial_count} iterations."
         msg += f" In total, {self.count} simulations are exported.\n"
         msg += f"Total wall time: {time() - self.start_time:.1f} s"
-
         _SimMonitor.reprint(msg, end="\n", flush=True)
 
     @staticmethod
     def reprint(msg, end="\n", flush=True):
-        """
-        Prints a message on the same line as the previous one and replaces the
-        previous message with the new one, deleting the extra characters from
-        the previous message.
+        """Prints a message replacing the previous line to avoid cluttering
+        the terminal output during concurrent simulation progress updates.
 
         Parameters
         ----------
@@ -1331,12 +1720,8 @@ def reprint(msg, end="\n", flush=True):
         -------
         None
         """
-
         padding = ""
-
         if len(msg) < _SimMonitor._last_print_len:
             padding = " " * (_SimMonitor._last_print_len - len(msg))
-
         print(msg + padding, end=end, flush=flush)
-
         _SimMonitor._last_print_len = len(msg)
diff --git a/rocketpy/stochastic/stochastic_model.py b/rocketpy/stochastic/stochastic_model.py
index 879b61e70..ca26f6578 100644
--- a/rocketpy/stochastic/stochastic_model.py
+++ b/rocketpy/stochastic/stochastic_model.py
@@ -550,6 +550,11 @@ def visualize_attributes(self):
         Model object. The report includes the variable name, the nominal value,
         the standard deviation, and the distribution function used to generate
         the random attributes.
+
+        Returns
+        -------
+        str
+            The formatted report. It is also printed for interactive use.
         """
 
         def format_attribute(attr, value):
@@ -630,4 +635,10 @@ def format_attribute(attr, value):
                 format_attribute(attr, attributes[attr]) for attr in custom_attributes
             )
 
-        print("\n".join(filter(None, report)))
+        # This is an explicit, user-invoked display method, so it prints
+        # unconditionally (like ``info``/``all_info`` elsewhere) rather than
+        # logging at INFO level, which is silenced by default. The report is
+        # also returned so it can be used programmatically.
+        report_str = "\n".join(filter(None, report))
+        print(report_str)
+        return report_str
diff --git a/rocketpy/stochastic/stochastic_parachute.py b/rocketpy/stochastic/stochastic_parachute.py
index 038907187..c0ad1ae1d 100644
--- a/rocketpy/stochastic/stochastic_parachute.py
+++ b/rocketpy/stochastic/stochastic_parachute.py
@@ -1,6 +1,6 @@
 """Defines the StochasticParachute class."""
 
-from rocketpy.rocket import Parachute
+from rocketpy.rocket import HemisphericalParachute
 
 from .stochastic_model import StochasticModel
 
@@ -148,4 +148,4 @@ def create_object(self):
             Parachute object with the randomly generated input arguments.
         """
         generated_dict = next(self.dict_generator())
-        return Parachute(**generated_dict)
+        return HemisphericalParachute(**generated_dict)
diff --git a/rocketpy/stochastic/stochastic_rocket.py b/rocketpy/stochastic/stochastic_rocket.py
index 794a66c85..87c479855 100644
--- a/rocketpy/stochastic/stochastic_rocket.py
+++ b/rocketpy/stochastic/stochastic_rocket.py
@@ -17,7 +17,7 @@
     TrapezoidalFins,
 )
 from rocketpy.rocket.components import Components
-from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.parachutes.parachute import Parachute
 from rocketpy.rocket.rocket import Rocket
 from rocketpy.stochastic.stochastic_generic_motor import StochasticGenericMotor
 from rocketpy.stochastic.stochastic_motor_model import StochasticMotorModel
@@ -362,7 +362,7 @@ def add_parachute(self, parachute):
         # checks if input is a StochasticParachute type
         if not isinstance(parachute, (Parachute, StochasticParachute)):
             raise TypeError(
-                "`parachute` must be of Parachute or StochasticParachute type"
+                "`parachute` must be of valid parachute model or StochasticParachute type"
             )
         if isinstance(parachute, Parachute):
             parachute = StochasticParachute(parachute=parachute)
@@ -795,13 +795,6 @@ def create_object(self):
 
         for parachute in self.parachutes:
             parachute = self._create_parachute(parachute)
-            rocket.add_parachute(
-                name=parachute.name,
-                cd_s=parachute.cd_s,
-                trigger=parachute.trigger,
-                sampling_rate=parachute.sampling_rate,
-                lag=parachute.lag,
-                noise=parachute.noise,
-            )
+            rocket.add_parachute(parachute=parachute)
 
         return rocket
diff --git a/rocketpy/tools.py b/rocketpy/tools.py
index 68ab3404a..a7e3582f6 100644
--- a/rocketpy/tools.py
+++ b/rocketpy/tools.py
@@ -11,6 +11,7 @@
 import importlib
 import importlib.metadata
 import json
+import logging
 import math
 import re
 import time
@@ -25,6 +26,8 @@
 from matplotlib.patches import Ellipse
 from packaging import version as packaging_version
 
+logger = logging.getLogger(__name__)
+
 # Mapping of module name and the name of the package that should be installed
 INSTALL_MAPPING = {"IPython": "ipython"}
 
@@ -1469,6 +1472,6 @@ def find_obj_from_hash(obj, hash_, depth_limit=None):
 
     res = doctest.testmod()
     if res.failed < 1:
-        print(f"All the {res.attempted} tests passed!")
+        logger.info("All the %d tests passed!", res.attempted)
     else:
-        print(f"{res.failed} out of {res.attempted} tests failed.")
+        logger.error("%d out of %d tests failed.", res.failed, res.attempted)
diff --git a/rocketpy/utilities.py b/rocketpy/utilities.py
index 09083339d..4c76180fb 100644
--- a/rocketpy/utilities.py
+++ b/rocketpy/utilities.py
@@ -1,10 +1,12 @@
 import inspect
 import json
+import logging
 import os
 import warnings
 from datetime import date
 from importlib.metadata import version
 from pathlib import Path
+from typing import TYPE_CHECKING
 
 import matplotlib.pyplot as plt
 import numpy as np
@@ -16,7 +18,60 @@
 from .mathutils.function import Function
 from .plots.plot_helpers import show_or_save_plot
 from .rocket.aero_surface import TrapezoidalFins
-from .simulation.flight import Flight
+
+if TYPE_CHECKING:  # pragma: no cover
+    from .simulation.flight import Flight
+
+
+def enable_logging(level="WARNING"):
+    """Enable RocketPy logging output to the console.
+
+    Attaches a StreamHandler to the ``rocketpy`` logger so that internal
+    runtime events (simulation progress, warnings, errors) are printed to
+    the terminal. Only RocketPy logs are affected — global/root logging
+    is not modified. By default, only WARNING and above are shown.
+
+    Parameters
+    ----------
+    level : str, optional
+        The minimum logging level to display. Options are "DEBUG", "INFO",
+        "WARNING", "ERROR", and "CRITICAL". Default is "WARNING".
+
+    Examples
+    --------
+    Show only warnings and errors (default):
+
+    >>> import rocketpy
+    >>> rocketpy.utilities.enable_logging()
+
+    Show all internal runtime messages, including simulation progress:
+
+    >>> import rocketpy
+    >>> rocketpy.utilities.enable_logging(level="DEBUG")
+
+    Show confirmations like "Simulation completed" and "File saved":
+
+    >>> import rocketpy
+    >>> rocketpy.utilities.enable_logging(level="INFO")
+    """
+    numeric_level = getattr(logging, level.upper(), None)
+    if not isinstance(numeric_level, int):
+        raise ValueError(f"Invalid logging level: '{level}'")
+
+    logger = logging.getLogger("rocketpy")
+
+    # Remove any existing StreamHandlers to avoid duplicate messages
+    logger.handlers = [
+        h for h in logger.handlers if not isinstance(h, logging.StreamHandler)
+    ]
+
+    logger.setLevel(numeric_level)
+
+    handler = logging.StreamHandler()
+    handler.setLevel(numeric_level)
+    handler.setFormatter(logging.Formatter("%(levelname)s | %(name)s | %(message)s"))
+
+    logger.addHandler(handler)
 
 
 def compute_cd_s_from_drop_test(
@@ -202,7 +257,43 @@ def du(z, u):
     return altitude_function, velocity_function, final_sol
 
 
-# pylint: disable=too-many-statements
+def calculate_stall_wind_velocity(flight, stall_angle):
+    """Calculate the maximum wind velocity before the angle of attack exceeds a
+    desired stall angle, at the instant of departing the launch rail.
+
+    Can be helpful if you know the exact stall angle of all aerodynamic
+    surfaces.
+
+    Parameters
+    ----------
+    flight : rocketpy.Flight
+        Flight object containing the rocket's flight data. Its
+        ``out_of_rail_velocity`` and ``inclination`` attributes are used.
+    stall_angle : float
+        Angle, in degrees, for which you would like to know the maximum wind
+        speed before the angle of attack exceeds it.
+
+    Returns
+    -------
+    float
+        Maximum wind velocity, in m/s, at rail departure before the angle of
+        attack exceeds ``stall_angle``.
+    """
+    v_f = flight.out_of_rail_velocity
+    theta = np.radians(flight.inclination)
+    stall_angle_rad = np.radians(stall_angle)
+
+    c = (np.cos(stall_angle_rad) ** 2 - np.cos(theta) ** 2) / np.sin(
+        stall_angle_rad
+    ) ** 2
+    w_v = (
+        2 * v_f * np.cos(theta) / c
+        + (4 * v_f * v_f * np.cos(theta) * np.cos(theta) / (c**2) + 4 * v_f * v_f / c)
+        ** 0.5
+    ) / 2
+    return w_v
+
+
 def fin_flutter_analysis(
     fin_thickness,
     shear_modulus,
@@ -231,8 +322,7 @@ def fin_flutter_analysis(
     see_prints : boolean, optional
         True if you want to see the prints, False otherwise.
     see_graphs : boolean, optional
-        True if you want to see the graphs, False otherwise. If False, the
-        function will return the vectors containing the data for the graphs.
+        True if you want to see the graphs, False otherwise.
     filename : str | None, optional
         The path the plot should be saved to. By default None, in which case the
         plot will be shown instead of saved. Supported file endings are: eps,
@@ -241,7 +331,12 @@ def fin_flutter_analysis(
 
     Return
     ------
-    None
+    flutter_mach : rocketpy.Function
+        The Mach Number at which the fin flutter occurs as a function of time,
+        considering the variation of the speed of sound with altitude.
+    safety_factor : rocketpy.Function
+        The Safety Factor for the fin flutter as a function of time, defined as
+        the flutter Mach Number divided by the freestream Mach Number.
     """
     found_fin = False
     surface_area = None
@@ -284,8 +379,12 @@ def fin_flutter_analysis(
         )
     if see_graphs:
         _flutter_plots(flight, flutter_mach, safety_factor, filename=filename)
-    else:
-        return flutter_mach, safety_factor
+
+    # Always return the computed results so callers can use the flutter margin
+    # programmatically. These are safety-critical numbers and must never be
+    # silently discarded (they were previously only returned when
+    # ``see_graphs=False`` and otherwise only logged at INFO level).
+    return flutter_mach, safety_factor
 
 
 def _flutter_mach_number(
@@ -428,18 +527,21 @@ def _flutter_prints(
     min_sf = safety_factor[time_index, 1]
     altitude_min_sf = flight.z(time_min_sf) - flight.env.elevation
 
-    print("\nFin's parameters")
-    print(f"Surface area (S): {surface_area:.4f} m2")
-    print(f"Aspect ratio (AR): {aspect_ratio:.3f}")
-    print(f"tip_chord/root_chord ratio = \u03bb = {lambda_:.3f}")
-    print(f"Fin Thickness: {fin_thickness:.5f} m")
-    print(f"Shear Modulus (G): {shear_modulus:.3e} Pa")
-
-    print("\nFin Flutter Analysis")
-    print(f"Minimum Fin Flutter Velocity: {min_vel:.3f} m/s at {time_min_mach:.2f} s")
-    print(f"Minimum Fin Flutter Mach Number: {min_mach:.3f} ")
-    print(f"Minimum Safety Factor: {min_sf:.3f} at {time_min_sf:.2f} s")
-    print(f"Altitude of minimum Safety Factor: {altitude_min_sf:.3f} m (AGL)\n")
+    # This is an explicit, opt-in report (gated on ``see_prints``), so it uses
+    # print() to display unconditionally rather than logging.info, which is
+    # silenced by default.
+    print(
+        f"Fin's parameters: Surface area (S)={surface_area:.4f} m2"
+        f" | AR={aspect_ratio:.3f} | \u03bb={lambda_:.3f}"
+        f" | Thickness={fin_thickness:.5f} m"
+        f" | Shear Modulus (G)={shear_modulus:.3e} Pa"
+    )
+    print(
+        f"Fin Flutter Analysis: Min flutter velocity={min_vel:.3f} m/s"
+        f" at t={time_min_mach:.2f} s | Min flutter Mach={min_mach:.3f}"
+        f" | Min safety factor={min_sf:.3f} at t={time_min_sf:.2f} s"
+        f" | Altitude of min safety factor={altitude_min_sf:.3f} m (AGL)"
+    )
 
 
 def apogee_by_mass(flight, min_mass, max_mass, points=10, plot=True):
@@ -477,6 +579,9 @@ def apogee_by_mass(flight, min_mass, max_mass, points=10, plot=True):
         Function object containing the estimated apogee as a function of the
         rocket's mass (without motor nor propellant).
     """
+    # Imported lazily to avoid a circular import (Flight imports utilities).
+    from .simulation.flight import Flight  # pylint: disable=import-outside-toplevel
+
     rocket = flight.rocket
 
     def apogee(mass):
@@ -547,6 +652,9 @@ def liftoff_speed_by_mass(flight, min_mass, max_mass, points=10, plot=True):
         Function object containing the estimated liftoff speed as a function of
         the rocket's mass (without motor nor propellant).
     """
+    # Imported lazily to avoid a circular import (Flight imports utilities).
+    from .simulation.flight import Flight  # pylint: disable=import-outside-toplevel
+
     rocket = flight.rocket
 
     def liftoff_speed(mass):
@@ -605,7 +713,7 @@ def get_instance_attributes(instance):
     return attributes_dict
 
 
-def save_to_rpy(flight: Flight, filename: str, include_outputs=False):
+def save_to_rpy(flight: "Flight", filename: str, include_outputs=False):
     """Saves a .rpy file into the given path, containing key simulation
     informations to reproduce the results.
 
diff --git a/tests/acceptance/test_bella_lui_rocket.py b/tests/acceptance/test_bella_lui_rocket.py
index bcfe325bc..54db9abac 100644
--- a/tests/acceptance/test_bella_lui_rocket.py
+++ b/tests/acceptance/test_bella_lui_rocket.py
@@ -6,7 +6,14 @@
 import numpy as np
 from scipy.signal import savgol_filter
 
-from rocketpy import Environment, Flight, Function, Rocket, SolidMotor
+from rocketpy import (
+    Environment,
+    Flight,
+    Function,
+    HemisphericalParachute,
+    Rocket,
+    SolidMotor,
+)
 
 mpl.rc("figure", max_open_warning=0)  # Prevent matplotlib warnings
 
@@ -67,6 +74,7 @@ def test_bella_lui_rocket_data_asserts_acceptance():
         type="Reanalysis",
         file="data/weather/bella_lui_weather_data_ERA5.nc",
         dictionary="ECMWF",
+        pressure_conversion_factor="hPa",
     )
     env.max_expected_height = 2000
 
@@ -131,7 +139,7 @@ def drogue_trigger(p, h, y):
         # activate drogue when vz < 0 m/s.
         return True if y[5] < 0 else False
 
-    BellaLui.add_parachute(
+    drogue = HemisphericalParachute(
         "Drogue",
         cd_s=parameters.get("CdS_drogue")[0],
         trigger=drogue_trigger,
@@ -139,6 +147,7 @@ def drogue_trigger(p, h, y):
         lag=parameters.get("lag_rec")[0],
         noise=(0, 8.3, 0.5),
     )
+    BellaLui.add_parachute(parachute=drogue)
 
     # Define aerodynamic drag coefficients
     power_off_drag_by_mach = Function(
diff --git a/tests/acceptance/test_ndrt_2020_rocket.py b/tests/acceptance/test_ndrt_2020_rocket.py
index 7874ee164..cd03b0012 100644
--- a/tests/acceptance/test_ndrt_2020_rocket.py
+++ b/tests/acceptance/test_ndrt_2020_rocket.py
@@ -3,7 +3,7 @@
 import pytest
 from scipy.signal import savgol_filter
 
-from rocketpy import Environment, Flight, Rocket, SolidMotor
+from rocketpy import Environment, Flight, HemisphericalParachute, Rocket, SolidMotor
 
 
 @pytest.mark.parametrize(
@@ -83,6 +83,7 @@ def test_ndrt_2020_rocket_data_asserts_acceptance(env_file):
         type="Reanalysis",
         file=env_file,
         dictionary="ECMWF",
+        pressure_conversion_factor="hPa",
     )
     env.max_expected_height = 2000
 
@@ -154,7 +155,7 @@ def main_trigger(p, h, y):  # pylint: disable=unused-argument
         # activate main when vz < 0 m/s and z < 167.64 m (AGL) or 550 ft (AGL)
         return True if y[5] < 0 and h < 167.64 else False
 
-    NDRT2020.add_parachute(
+    drogue = HemisphericalParachute(
         "Drogue",
         cd_s=parameters.get("cd_s_drogue")[0],
         trigger=drogue_trigger,
@@ -162,7 +163,7 @@ def main_trigger(p, h, y):  # pylint: disable=unused-argument
         lag=parameters.get("lag_rec")[0],
         noise=(0, 8.3, 0.5),
     )
-    NDRT2020.add_parachute(
+    main = HemisphericalParachute(
         "Main",
         cd_s=parameters.get("cd_s_main")[0],
         trigger=main_trigger,
@@ -170,6 +171,8 @@ def main_trigger(p, h, y):  # pylint: disable=unused-argument
         lag=parameters.get("lag_rec")[0],
         noise=(0, 8.3, 0.5),
     )
+    NDRT2020.add_parachute(parachute=drogue)
+    NDRT2020.add_parachute(parachute=main)
 
     # Flight
     rocketpy_flight = Flight(
diff --git a/tests/fixtures/environment/environment_fixtures.py b/tests/fixtures/environment/environment_fixtures.py
index 818f434c7..5a3f3cd64 100644
--- a/tests/fixtures/environment/environment_fixtures.py
+++ b/tests/fixtures/environment/environment_fixtures.py
@@ -111,6 +111,7 @@ def environment_spaceport_america_2023():
         type="Reanalysis",
         file="data/weather/spaceport_america_pressure_levels_2023_hourly.nc",
         dictionary="ECMWF",
+        pressure_conversion_factor="hPa",
     )
 
     env.max_expected_height = 6000
diff --git a/tests/fixtures/monte_carlo/stochastic_fixtures.py b/tests/fixtures/monte_carlo/stochastic_fixtures.py
index 6610666cf..94490ce77 100644
--- a/tests/fixtures/monte_carlo/stochastic_fixtures.py
+++ b/tests/fixtures/monte_carlo/stochastic_fixtures.py
@@ -240,8 +240,8 @@ def stochastic_calisto(
     rocket.set_rail_buttons(
         stochastic_rail_buttons, lower_button_position=(-0.618, 0.001, "normal")
     )
-    rocket.add_parachute(stochastic_main_parachute)
-    rocket.add_parachute(stochastic_drogue_parachute)
+    rocket.add_parachute(parachute=stochastic_main_parachute)
+    rocket.add_parachute(parachute=stochastic_drogue_parachute)
     return rocket
 
 
diff --git a/tests/fixtures/motor/tanks_fixtures.py b/tests/fixtures/motor/tanks_fixtures.py
index 88721966d..aba5f5a7e 100644
--- a/tests/fixtures/motor/tanks_fixtures.py
+++ b/tests/fixtures/motor/tanks_fixtures.py
@@ -499,7 +499,7 @@ def temperature(t):
 
     return MassBasedTank(
         name="Variable Density N2O Tank",
-        geometry=CylindricalTank(height=0.8, radius=0.06, spherical_caps=True),
+        geometry=CylindricalTank(height=0.8, radius_function=0.06, spherical_caps=True),
         flux_time=7,
         liquid=nitrous_oxide_non_constant_fluid,
         gas=nitrous_oxide_non_constant_fluid,
diff --git a/tests/fixtures/parachutes/parachute_fixtures.py b/tests/fixtures/parachutes/parachute_fixtures.py
index 9723cda8e..c74fab648 100644
--- a/tests/fixtures/parachutes/parachute_fixtures.py
+++ b/tests/fixtures/parachutes/parachute_fixtures.py
@@ -1,6 +1,6 @@
 import pytest
 
-from rocketpy import Parachute
+from rocketpy import HemisphericalParachute
 
 
 @pytest.fixture
@@ -52,7 +52,7 @@ def calisto_main_chute(calisto_main_parachute_trigger):
     rocketpy.Parachute
         The main parachute of the Calisto rocket.
     """
-    return Parachute(
+    return HemisphericalParachute(
         name="calisto_main_chute",
         cd_s=10.0,
         trigger=calisto_main_parachute_trigger,
@@ -77,7 +77,7 @@ def calisto_drogue_chute(calisto_drogue_parachute_trigger):
     rocketpy.Parachute
         The drogue parachute of the Calisto rocket.
     """
-    return Parachute(
+    return HemisphericalParachute(
         name="calisto_drogue_chute",
         cd_s=1.0,
         trigger=calisto_drogue_parachute_trigger,
diff --git a/tests/fixtures/rockets/rocket_fixtures.py b/tests/fixtures/rockets/rocket_fixtures.py
index 9cb3caa3c..55ebd7165 100644
--- a/tests/fixtures/rockets/rocket_fixtures.py
+++ b/tests/fixtures/rockets/rocket_fixtures.py
@@ -1,7 +1,7 @@
 import numpy as np
 import pytest
 
-from rocketpy import Rocket
+from rocketpy import HemisphericalParachute, Rocket
 
 
 @pytest.fixture
@@ -404,14 +404,18 @@ def prometheus_cd_at_ma(mach):
         position=0.273,
         sweep_length=0.066,
     )
-    prometheus.add_parachute(
+    drogue = HemisphericalParachute(
         "Drogue",
         cd_s=1.6 * np.pi * 0.3048**2,  # Cd = 1.6, D_chute = 24 in
         trigger="apogee",
+        sampling_rate=100,
     )
-    prometheus.add_parachute(
+    main = HemisphericalParachute(
         "Main",
         cd_s=2.2 * np.pi * 0.9144**2,  # Cd = 2.2, D_chute = 72 in
         trigger=457.2,  # 1500 ft
+        sampling_rate=100,
     )
+    prometheus.add_parachute(parachute=drogue)
+    prometheus.add_parachute(parachute=main)
     return prometheus
diff --git a/tests/fixtures/surfaces/surface_fixtures.py b/tests/fixtures/surfaces/surface_fixtures.py
index c48627478..3819595dc 100644
--- a/tests/fixtures/surfaces/surface_fixtures.py
+++ b/tests/fixtures/surfaces/surface_fixtures.py
@@ -1,11 +1,14 @@
 import pytest
 
 from rocketpy.rocket.aero_surface import (
+    EllipticalFin,
     EllipticalFins,
+    FreeFormFin,
     FreeFormFins,
     NoseCone,
     RailButtons,
     Tail,
+    TrapezoidalFin,
     TrapezoidalFins,
 )
 
@@ -69,6 +72,29 @@ def calisto_trapezoidal_fins():
     )
 
 
+@pytest.fixture
+def calisto_trapezoidal_fin():
+    """A single trapezoidal fin based on Calisto dimensions.
+
+    Returns
+    -------
+    rocketpy.TrapezoidalFin
+        A single trapezoidal fin.
+    """
+    return TrapezoidalFin(
+        angular_position=0,
+        span=0.100,
+        root_chord=0.120,
+        tip_chord=0.040,
+        rocket_radius=0.0635,
+        name="calisto_trapezoidal_fin",
+        cant_angle=0,
+        sweep_length=None,
+        sweep_angle=None,
+        airfoil=None,
+    )
+
+
 @pytest.fixture
 def calisto_trapezoidal_fins_custom_sweep_length():
     """The trapezoidal fins of the Calisto rocket with
@@ -130,6 +156,23 @@ def calisto_free_form_fins():
     )
 
 
+@pytest.fixture
+def calisto_free_form_fin():
+    """A single free-form fin based on Calisto-like dimensions.
+
+    Returns
+    -------
+    rocketpy.FreeFormFin
+        A single free-form fin.
+    """
+    return FreeFormFin(
+        angular_position=0,
+        shape_points=[(0, 0), (0.08, 0.1), (0.12, 0.1), (0.12, 0)],
+        rocket_radius=0.0635,
+        name="calisto_free_form_fin",
+    )
+
+
 @pytest.fixture
 def calisto_rail_buttons():
     """The rail buttons of the Calisto rocket.
@@ -157,3 +200,23 @@ def elliptical_fin_set():
         airfoil=None,
         name="Test Elliptical Fins",
     )
+
+
+@pytest.fixture
+def calisto_elliptical_fin():
+    """A single elliptical fin based on Calisto-like dimensions.
+
+    Returns
+    -------
+    rocketpy.EllipticalFin
+        A single elliptical fin.
+    """
+    return EllipticalFin(
+        angular_position=0,
+        span=0.100,
+        root_chord=0.120,
+        rocket_radius=0.0635,
+        cant_angle=0,
+        airfoil=None,
+        name="calisto_elliptical_fin",
+    )
diff --git a/tests/fixtures/utilities/flight_calisto_robust.rpy b/tests/fixtures/utilities/flight_calisto_robust.rpy
index 74da896cb..3149e43b4 100644
--- a/tests/fixtures/utilities/flight_calisto_robust.rpy
+++ b/tests/fixtures/utilities/flight_calisto_robust.rpy
@@ -1,6 +1,6 @@
 {
-  "date": "2025-03-28",
-  "version": "1.8.0",
+  "date": "2026-05-07",
+  "version": "1.12.1",
   "simulation": {
     "rocket": {
       "radius": 0.0635,
@@ -12,23229 +12,10154 @@
       "I_13_without_motor": 0,
       "I_23_without_motor": 0,
       "power_off_drag": {
-        "source": [
-          [
-            0.01,
-            0.333865758
+        "source": "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+        "title": null,
+        "inputs": [
+          "alpha",
+          "beta",
+          "mach",
+          "reynolds",
+          "pitch_rate",
+          "yaw_rate",
+          "roll_rate"
+        ],
+        "outputs": [
+          "Drag Coefficient with Power Off"
+        ],
+        "interpolation": null,
+        "extrapolation": null,
+        "signature": {
+          "module": "rocketpy.mathutils.function",
+          "name": "Function",
+          "hash": 8532846258036
+        }
+      },
+      "power_on_drag": {
+        "source": 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+        "title": null,
+        "inputs": [
+          "alpha",
+          "beta",
+          "mach",
+          "reynolds",
+          "pitch_rate",
+          "yaw_rate",
+          "roll_rate"
+        ],
+        "outputs": [
+          "Drag Coefficient with Power On"
+        ],
+        "interpolation": null,
+        "extrapolation": null,
+        "signature": {
+          "module": "rocketpy.mathutils.function",
+          "name": "Function",
+          "hash": 8532846257868
+        }
+      },
+      "center_of_mass_without_motor": 0,
+      "coordinate_system_orientation": "tail_to_nose",
+      "motor": {
+        "thrust_source": {
+          "source": [
+            [
+              0.0,
+              0.0
+            ],
+            [
+              0.055,
+              100.0
+            ],
+            [
+              0.092,
+              1500.0
+            ],
+            [
+              0.1,
+              2000.0
+            ],
+            [
+              0.15,
+              2200.0
+            ],
+            [
+              0.2,
+              1800.0
+            ],
+            [
+              0.5,
+              1950.0
+            ],
+            [
+              1.0,
+              2034.0
+            ],
+            [
+              1.5,
+              2000.0
+            ],
+            [
+              2.0,
+              1900.0
+            ],
+            [
+              2.5,
+              1760.0
+            ],
+            [
+              2.9,
+              1700.0
+            ],
+            [
+              3.0,
+              1650.0
+            ],
+            [
+              3.3,
+              530.0
+            ],
+            [
+              3.4,
+              350.0
+            ],
+            [
+              3.9,
+              0.0
+            ]
           ],
-          [
-            0.02,
-            0.394981721
+          "title": "Thrust (N) x Time (S)",
+          "inputs": [
+            "Time (s)"
           ],
-          [
-            0.03,
-            0.407756063
+          "outputs": [
+            "Thrust (N)"
           ],
+          "interpolation": "linear",
+          "extrapolation": "zero",
+          "signature": {
+            "module": "rocketpy.mathutils.function",
+            "name": "Function",
+            "hash": 8532849063757
+          }
+        },
+        "dry_I_11": 0.125,
+        "dry_I_22": 0.125,
+        "dry_I_33": 0.002,
+        "dry_I_12": 0,
+        "dry_I_13": 0,
+        "dry_I_23": 0,
+        "nozzle_radius": 0.033,
+        "nozzle_area": 0.003421194399759285,
+        "center_of_dry_mass_position": 0.317,
+        "dry_mass": 1.815,
+        "nozzle_position": 0,
+        "burn_time": [
+          0,
+          3.9
+        ],
+        "interpolate": "linear",
+        "coordinate_system_orientation": "nozzle_to_combustion_chamber",
+        "reference_pressure": null,
+        "throat_radius": 0.011,
+        "grain_number": 5,
+        "grain_density": 1815,
+        "grain_outer_radius": 0.033,
+        "grain_initial_inner_radius": 0.015,
+        "grain_initial_height": 0.12,
+        "grain_separation": 0.005,
+        "grains_center_of_mass_position": 0.397,
+        "only_radial_burn": false,
+        "signature": {
+          "module": "rocketpy.motors.solid_motor",
+          "name": "SolidMotor",
+          "hash": 8532846656120
+        }
+      },
+      "motor_position": -1.373,
+      "aerodynamic_surfaces": [
+        [
+          {
+            "_length": 0.55829,
+            "_kind": "vonkarman",
+            "_base_radius": 0.0635,
+            "_bluffness": null,
+            "_rocket_radius": 0.0635,
+            "_power": null,
+            "name": "calisto_nose_cone",
+            "signature": {
+              "module": "rocketpy.rocket.aero_surface.nose_cone",
+              "name": "NoseCone",
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-      "title": "Ay (M/S\u00b2) x Time (S)",
-      "inputs": [
-        "Time (s)"
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-      "outputs": [
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-      "interpolation": "spline",
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-      "signature": {
-        "module": "rocketpy.mathutils.function",
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-      "title": "\u03912 (Rad/S\u00b2) x Time (S)",
-      "inputs": [
-        "Time (s)"
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-      "outputs": [
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-      "signature": {
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+      "title": "\u03913 (Rad/S\u00b2) x Time (S)",
+      "inputs": [
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+      "outputs": [
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+          160.93396185705825,
           0.0
         ],
         [
-          161.5801713796893,
+          161.05499742452804,
           0.0
         ],
         [
-          161.73657554616506,
+          161.17603299199783,
           0.0
         ],
         [
-          161.89297971264082,
+          161.29706855946762,
           0.0
         ],
         [
-          162.11653214894974,
+          161.46985652170034,
           0.0
         ],
         [
-          162.34008458525867,
+          161.64264448393305,
           0.0
         ],
         [
-          162.5636370215676,
+          161.81543244616577,
           0.0
         ],
         [
-          162.7871894578765,
+          161.9882204083985,
           0.0
         ],
         [
-          163.01074189418543,
+          162.1610083706312,
           0.0
         ],
         [
-          163.3020518484637,
+          162.38610275126362,
           0.0
         ],
         [
-          163.59336180274195,
+          162.61119713189603,
           0.0
         ],
         [
-          163.88467175702021,
+          162.83629151252845,
           0.0
         ],
         [
-          164.17598171129848,
+          163.06138589316086,
           0.0
         ],
         [
-          164.4850936705858,
+          163.3001953672972,
           0.0
         ],
         [
-          164.79420562987312,
+          163.53900484143352,
           0.0
         ],
         [
-          165.10331758916044,
+          163.77781431556986,
           0.0
         ],
         [
-          165.4129391221861,
+          164.01699558831393,
           0.0
         ],
         [
-          165.72256065521174,
+          164.256176861058,
           0.0
         ],
         [
-          166.03218218823739,
+          164.49535813380209,
           0.0
         ],
         [
-          166.34184757413777,
+          164.73455176863084,
           0.0
         ],
         [
-          167.93141144685217,
+          165.96552936083825,
           0.0
         ],
         [
-          169.52097531956656,
+          167.19650695304566,
           0.0
         ],
         [
-          171.11053919228095,
+          168.42748454525307,
           0.0
         ],
         [
-          175.76088994831585,
+          172.0340398974043,
           0.0
         ],
         [
-          180.41124070435075,
+          175.64059524955556,
           0.0
         ],
         [
-          185.06159146038564,
+          179.2471506017068,
           0.0
         ],
         [
-          202.12571753179242,
+          196.48491242496618,
           0.0
         ],
         [
-          219.1898436031992,
+          213.72267424822556,
           0.0
         ],
         [
-          236.25396967460597,
+          230.96043607148493,
           0.0
         ],
         [
-          261.9195710352043,
+          256.216460721343,
           0.0
         ],
         [
-          287.5851723958026,
+          281.4724853712011,
           0.0
         ],
         [
-          298.2290954115797,
+          298.21839993404154,
           0.0
         ]
       ],
-      "title": "M3 (Nm) x Time (S)",
+      "title": "Net Thrust (N) x Time (S)",
       "inputs": [
         "Time (s)"
       ],
       "outputs": [
-        "M3 (Nm)"
+        "Net Thrust (N)"
       ],
       "interpolation": "linear",
       "extrapolation": "zero",
       "signature": {
         "module": "rocketpy.mathutils.function",
-        "name": "Function"
+        "name": "Function",
+        "hash": 8532846656111
       }
     },
     "signature": {
       "module": "rocketpy.simulation.flight",
-      "name": "Flight"
+      "name": "Flight",
+      "hash": 8532846519592
     }
   }
 }
\ No newline at end of file
diff --git a/tests/integration/environment/test_environment.py b/tests/integration/environment/test_environment.py
index 5802650dc..d51551397 100644
--- a/tests/integration/environment/test_environment.py
+++ b/tests/integration/environment/test_environment.py
@@ -1,5 +1,5 @@
 import time
-from datetime import date, datetime, timezone
+from datetime import date, datetime, timedelta, timezone
 from unittest.mock import patch
 
 import numpy as np
@@ -41,6 +41,21 @@ def test_era5_atmosphere(mock_show, example_spaceport_env):  # pylint: disable=u
         Example environment object to be tested.
     """
     example_spaceport_env.set_date((2018, 10, 15, 12))
+    example_spaceport_env.set_atmospheric_model(
+        type="Reanalysis",
+        file="data/weather/SpaceportAmerica_2018_ERA-5.nc",
+        dictionary="ECMWF",
+        pressure_conversion_factor="hPa",
+    )
+    assert example_spaceport_env.all_info() is None
+
+
+@patch("matplotlib.pyplot.show")
+def test_era5_atmosphere_auto_detect_pressure(mock_show, example_spaceport_env):  # pylint: disable=unused-argument
+    """Tests the Reanalysis model with the ERA5 file using the default
+    pressure_conversion_factor=None (auto-detection).
+    """
+    example_spaceport_env.set_date((2018, 10, 15, 12))
     example_spaceport_env.set_atmospheric_model(
         type="Reanalysis",
         file="data/weather/SpaceportAmerica_2018_ERA-5.nc",
@@ -146,6 +161,7 @@ def test_wind_plots_wrapping_direction(mock_show, example_plain_env):  # pylint:
     assert example_plain_env.plots.atmospheric_model() is None
 
 
+@pytest.mark.slow
 @pytest.mark.parametrize(
     "model_name",
     [
@@ -195,6 +211,42 @@ def test_gfs_atmosphere(mock_show, example_spaceport_env):  # pylint: disable=un
     assert example_spaceport_env.all_info() is None
 
 
+@pytest.mark.slow
+@patch("matplotlib.pyplot.show")
+def test_aigfs_atmosphere(mock_show, example_spaceport_env):  # pylint: disable=unused-argument
+    """Tests the Forecast model with the AIGFS file.
+
+    Parameters
+    ----------
+    mock_show : mock
+        Mock object to replace matplotlib.pyplot.show() method.
+    example_spaceport_env : rocketpy.Environment
+        Example environment object to be tested.
+    """
+    example_spaceport_env.set_atmospheric_model(type="Forecast", file="AIGFS")
+    assert example_spaceport_env.all_info() is None
+
+
+@pytest.mark.slow
+@patch("matplotlib.pyplot.show")
+def test_hrrr_atmosphere(mock_show, example_spaceport_env):  # pylint: disable=unused-argument
+    """Tests the Forecast model with the HRRR file.
+
+    Parameters
+    ----------
+    mock_show : mock
+        Mock object to replace matplotlib.pyplot.show() method.
+    example_spaceport_env : rocketpy.Environment
+        Example environment object to be tested.
+    """
+    # Sometimes the HRRR latest-model can fail due to not having at least 24
+    # hours in the future in the forecast, so we try with 12 hours in the future
+    # only.
+    example_spaceport_env.set_date(datetime.now() + timedelta(hours=12))
+    example_spaceport_env.set_atmospheric_model(type="Forecast", file="HRRR")
+    assert example_spaceport_env.all_info() is None
+
+
 @pytest.mark.slow
 @patch("matplotlib.pyplot.show")
 def test_nam_atmosphere(mock_show, example_spaceport_env):  # pylint: disable=unused-argument
@@ -256,21 +308,27 @@ def test_wyoming_sounding_atmosphere(mock_show, example_plain_env):  # pylint: d
 
     # TODO:: this should be added to the set_atmospheric_model() method as a
     #        "file" option, instead of receiving the URL as a string.
-    url = "http://weather.uwyo.edu/cgi-bin/sounding?region=samer&TYPE=TEXT%3ALIST&YEAR=2019&MONTH=02&FROM=0500&TO=0512&STNM=83779"
-    # give it at least 5 times to try to download the file
+    url = (
+        "https://weather.uwyo.edu/wsgi/sounding?"
+        "datetime=2019-02-05+00:00:00&id=83779&type=TEXT:LIST"
+    )
+    # give it at least 5 times to try to download the file, then skip instead
+    # of silently keeping the standard atmosphere and failing the assertions
     for i in range(5):
         try:
             example_plain_env.set_atmospheric_model(type="wyoming_sounding", file=url)
             break
         except Exception:  # pylint: disable=broad-except
             time.sleep(2**i)
+    else:
+        pytest.skip("Could not fetch Wyoming sounding data from weather.uwyo.edu")
     assert example_plain_env.all_info() is None
     assert abs(example_plain_env.pressure(0) - 93600.0) < 1e-8
     assert (
         abs(example_plain_env.barometric_height(example_plain_env.pressure(0)) - 722.0)
         < 1e-8
     )
-    assert abs(example_plain_env.wind_velocity_x(0) - -2.9005178894925043) < 1e-8
+    assert abs(example_plain_env.wind_velocity_x(0) - -2.9130471244363165) < 1e-8
     assert abs(example_plain_env.temperature(100) - 291.75) < 1e-8
 
 
diff --git a/tests/integration/motors/test_ring_cluster_motor.py b/tests/integration/motors/test_ring_cluster_motor.py
new file mode 100644
index 000000000..413169ae7
--- /dev/null
+++ b/tests/integration/motors/test_ring_cluster_motor.py
@@ -0,0 +1,253 @@
+# pylint: disable=invalid-name
+import numpy as np
+import pytest
+
+from rocketpy import Flight, Function, SolidMotor
+from rocketpy.motors.ring_cluster_motor import RingClusterMotor
+
+
+@pytest.fixture
+def base_motor():
+    """
+    Creates a simplified SolidMotor for testing purposes.
+    Properties:
+    - Constant Thrust: 1000 N
+    - Burn time: 5 s
+    - Dry mass: 10 kg
+    - Dry Inertia: (1.0, 1.0, 0.1)
+    """
+    thrust_curve = Function(lambda t: 1000 if t < 5 else 0, "Time (s)", "Thrust (N)")
+
+    return SolidMotor(
+        thrust_source=thrust_curve,
+        burn_time=5,
+        dry_mass=10.0,
+        dry_inertia=(1.0, 1.0, 0.1),  # Ixx, Iyy, Izz
+        grain_number=1,
+        grain_density=1000,
+        grain_outer_radius=0.05,
+        grain_initial_inner_radius=0.02,
+        grain_initial_height=0.5,
+        coordinate_system_orientation="nozzle_to_combustion_chamber",
+        nozzle_radius=0.02,
+        grain_separation=0.001,
+        grains_center_of_mass_position=0.25,
+        center_of_dry_mass_position=0.25,
+    )
+
+
+def test_cluster_initialization(base_motor):
+    """
+    Tests if the ClusterMotor initializes basic attributes correctly.
+    """
+    N = 3
+    R = 0.5
+    cluster = RingClusterMotor(motor=base_motor, number=N, radius=R)
+
+    assert cluster.number == N
+    assert cluster.radius == R
+    assert cluster.grain_outer_radius == base_motor.grain_outer_radius
+
+
+def test_cluster_mass_and_thrust_scaling(base_motor):
+    """
+    Tests if scalar and derived properties are correctly multiplied by N and that functional properties preserve their Function behavior
+    """
+    N = 4
+    R = 0.2
+    cluster = RingClusterMotor(motor=base_motor, number=N, radius=R)
+
+    assert np.isclose(cluster.thrust(1), base_motor.thrust(1) * N)
+
+    assert np.isclose(cluster.dry_mass, base_motor.dry_mass * N)
+
+    assert np.isclose(cluster.propellant_mass(0), base_motor.propellant_mass(0) * N)  # pylint: disable=not-callable
+    assert np.isclose(cluster.total_impulse, base_motor.total_impulse * N)
+    assert np.isclose(cluster.average_thrust, base_motor.average_thrust * N)
+
+
+def test_cluster_dry_inertia_steiner_theorem(base_motor):
+    """
+    Tests the implementation of the Parallel Axis Theorem (Huygens-Steiner)
+    for the static (dry) mass of the cluster.
+
+    Theoretical Formulas:
+    I_zz_cluster = N * I_zz_local + N * m * R^2
+    I_xx_cluster = N * I_xx_local + (N/2) * m * R^2  (Radial symmetry approximation)
+    """
+    N = 3
+    R = 1.0
+    cluster = RingClusterMotor(motor=base_motor, number=N, radius=R)
+
+    m_dry = base_motor.dry_mass
+    Ixx_loc = base_motor.dry_I_11
+    Izz_loc = base_motor.dry_I_33
+
+    expected_Izz = N * Izz_loc + N * m_dry * (R**2)
+
+    expected_I_trans = N * Ixx_loc + (N / 2) * m_dry * (R**2)
+
+    assert np.isclose(cluster.dry_I_33, expected_Izz)
+    assert np.isclose(cluster.dry_I_11, expected_I_trans)
+    assert np.isclose(cluster.dry_I_22, expected_I_trans)
+
+
+def test_cluster_invalid_inputs(base_motor):
+    """Tests if the validation raises errors for bad inputs."""
+    with pytest.raises(ValueError):
+        RingClusterMotor(motor=base_motor, number=1, radius=0.5)
+    with pytest.raises(ValueError):
+        RingClusterMotor(motor=base_motor, number=2, radius=-1.0)
+    with pytest.raises(TypeError):
+        RingClusterMotor(motor=base_motor, number="two", radius=0.5)
+
+
+def test_cluster_methods_and_setters(base_motor):
+    """Touches the display methods and setters to ensure coverage."""
+    cluster = RingClusterMotor(motor=base_motor, number=2, radius=0.5)
+
+    cluster.info()
+
+    cluster.draw_cluster_layout(show=False)
+    cluster.draw_cluster_layout(rocket_radius=0.1, show=False)
+
+    cluster.propellant_mass = 50.0
+    assert cluster.propellant_mass == 50.0
+    cluster.propellant_I_11 = 2.0
+    assert cluster.propellant_I_11 == 2.0
+
+
+def test_cluster_propellant_inertia_dynamic(base_motor):
+    """
+    Tests if the Steiner theorem is correctly applied dynamically
+    via exact geometric summation, especially for N=2.
+    """
+    N = 2
+    R = 0.5
+    cluster = RingClusterMotor(motor=base_motor, number=N, radius=R)
+
+    t = 0
+
+    m_prop = base_motor.propellant_mass(t)
+    Ixx_prop_loc = base_motor.propellant_I_11(t)
+    Izz_prop_loc = base_motor.propellant_I_33(t)
+
+    expected_ixx = (Ixx_prop_loc * N) + 0
+
+    expected_izz = (Izz_prop_loc * N) + (m_prop * N * R**2)
+
+    assert np.isclose(cluster.propellant_I_11(t), expected_ixx)  # pylint: disable=not-callable
+    assert np.isclose(cluster.propellant_I_33(t), expected_izz)
+
+
+def test_ring_cluster_motor_full_flight(
+    calisto_motorless,
+    calisto_nose_cone,
+    calisto_tail,
+    calisto_trapezoidal_fins,
+    example_plain_env,
+):
+    """Integration test for PR #924: a ``RingClusterMotor`` must work
+    end-to-end when mounted on a ``Rocket`` and flown to apogee. The clustered
+    motor scales the base motor's thrust and total impulse by the number of
+    motors, and the rocket must reach a positive apogee.
+
+    A lightweight base motor is used on purpose so the Calisto airframe stays
+    aerodynamically stable (positive static margin) with the extra aft mass.
+    """
+    # Lightweight base motor so the clustered aft mass keeps the rocket stable.
+    base = SolidMotor(
+        thrust_source=lambda t: 800 if t < 3 else 0,
+        burn_time=3,
+        dry_mass=0.2,
+        dry_inertia=(0.01, 0.01, 0.001),
+        grain_number=1,
+        grain_density=1700,
+        grain_outer_radius=0.02,
+        grain_initial_inner_radius=0.01,
+        grain_initial_height=0.1,
+        nozzle_radius=0.01,
+        grain_separation=0.001,
+        grains_center_of_mass_position=0.1,
+        center_of_dry_mass_position=0.1,
+        coordinate_system_orientation="nozzle_to_combustion_chamber",
+    )
+    number = 2
+    cluster = RingClusterMotor(motor=base, number=number, radius=0.03)
+
+    # Clustered thrust / total impulse scale with the number of motors.
+    assert np.isclose(cluster.thrust(1), base.thrust(1) * number)
+    assert np.isclose(cluster.total_impulse, base.total_impulse * number)
+
+    rocket = calisto_motorless
+    rocket.add_motor(cluster, position=-1.373)
+    # Add all aerodynamic surfaces at once so the intermediate (fin-less) state
+    # is never evaluated as unstable during construction.
+    rocket.add_surfaces(
+        [calisto_nose_cone, calisto_tail, calisto_trapezoidal_fins],
+        [1.160, -1.313, -1.168],
+    )
+    rocket.set_rail_buttons(
+        upper_button_position=0.082,
+        lower_button_position=-0.618,
+        angular_position=0,
+    )
+
+    # The clustered motor keeps the rocket aerodynamically stable.
+    assert rocket.static_margin(0) > 0
+
+    flight = Flight(
+        rocket=rocket,
+        environment=example_plain_env,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+        terminate_on_apogee=True,
+    )
+
+    assert flight.rocket.motor is cluster
+    assert flight.t_final > 0
+    assert flight.apogee > flight.env.elevation
+
+
+def test_cluster_transverse_inertia_asymmetry(base_motor):
+    """For N=2 the ring cluster is not axisymmetric, so the assembled I_22 must
+    differ from I_11. For a symmetric N=4 arrangement they must match. The base
+    Motor.I_22 previously returned I_11 unconditionally, which was wrong for the
+    N=2 case the class was specifically designed to handle."""
+    cluster_2 = RingClusterMotor(motor=base_motor, number=2, radius=0.5)
+    assert not np.isclose(cluster_2.I_22(1.0), cluster_2.I_11(1.0))
+
+    cluster_4 = RingClusterMotor(motor=base_motor, number=4, radius=0.5)
+    assert np.isclose(cluster_4.I_22(1.0), cluster_4.I_11(1.0))
+
+
+def test_cluster_scales_nozzle_area_and_forwards_reference_pressure():
+    """The cluster must forward the base motor's reference_pressure and scale
+    the nozzle exit area by the number of motors, so the pressure-thrust
+    correction stays consistent with the N-scaled thrust."""
+    thrust_curve = Function(lambda t: 1000 if t < 5 else 0, "Time (s)", "Thrust (N)")
+    motor = SolidMotor(
+        thrust_source=thrust_curve,
+        burn_time=5,
+        dry_mass=10.0,
+        dry_inertia=(1.0, 1.0, 0.1),
+        grain_number=1,
+        grain_density=1000,
+        grain_outer_radius=0.05,
+        grain_initial_inner_radius=0.02,
+        grain_initial_height=0.5,
+        coordinate_system_orientation="nozzle_to_combustion_chamber",
+        nozzle_radius=0.02,
+        grain_separation=0.001,
+        grains_center_of_mass_position=0.25,
+        center_of_dry_mass_position=0.25,
+        reference_pressure=101325,
+    )
+    number = 3
+    cluster = RingClusterMotor(motor=motor, number=number, radius=0.2)
+
+    assert cluster.reference_pressure == 101325
+    assert np.isclose(cluster.nozzle_area, np.pi * motor.nozzle_radius**2 * number)
+    # Vacuum thrust must be N times the single-motor vacuum thrust.
+    assert np.isclose(cluster.vacuum_thrust(1), motor.vacuum_thrust(1) * number)
diff --git a/tests/integration/motors/test_solid_motor.py b/tests/integration/motors/test_solid_motor.py
index b2b06409c..46638cca1 100644
--- a/tests/integration/motors/test_solid_motor.py
+++ b/tests/integration/motors/test_solid_motor.py
@@ -56,3 +56,32 @@ def test_evaluate_geometry_updates_properties(cesaroni_m1670):
 
     # evaluate at intermediate time
     assert isinstance(motor.grain_inner_radius(0.5), float)
+
+
+def test_only_radial_burn_grain_geometry_time_evolution(cesaroni_m1670):
+    """Regression for PR #944 (corrected Jacobian of the ``only_radial_burn``
+    branch of ``evaluate_geometry``).
+
+    With radial-only burning the integrated grain geometry over the full burn
+    must have a constant grain height (no axial regression) and a monotonically
+    growing inner radius, bounded by the initial inner radius and the grain
+    outer radius. A wrong Jacobian corrupts this integration.
+    """
+    motor = cesaroni_m1670
+    motor.only_radial_burn = True
+    motor.evaluate_geometry()
+
+    times = np.linspace(0, motor.grain_burn_out, 30)
+    heights = np.array([motor.grain_height(t) for t in times])
+    radii = np.array([motor.grain_inner_radius(t) for t in times])
+
+    # Radial-only burn: grain height stays at its initial value the whole burn.
+    assert np.allclose(heights, motor.grain_initial_height, atol=1e-9)
+
+    # Inner radius grows monotonically (non-decreasing) and actually increases.
+    assert np.all(np.diff(radii) >= -1e-12)
+    assert radii[-1] > radii[0]
+
+    # Physical bounds on the inner radius.
+    assert np.isclose(radii[0], motor.grain_initial_inner_radius)
+    assert radii[-1] <= motor.grain_outer_radius + 1e-12
diff --git a/tests/integration/simulation/test_flight.py b/tests/integration/simulation/test_flight.py
index 66f0848a4..a69729e2f 100644
--- a/tests/integration/simulation/test_flight.py
+++ b/tests/integration/simulation/test_flight.py
@@ -4,7 +4,7 @@
 import numpy as np
 import pytest
 
-from rocketpy import Flight
+from rocketpy import Flight, HemisphericalParachute
 
 plt.rcParams.update({"figure.max_open_warning": 0})
 
@@ -149,7 +149,7 @@ def test_simpler_parachute_triggers(mock_show, example_plain_env, calisto_robust
     """
     calisto_robust.parachutes = []
 
-    _ = calisto_robust.add_parachute(
+    main = HemisphericalParachute(
         "Main",
         cd_s=10.0,
         trigger=400,
@@ -157,7 +157,7 @@ def test_simpler_parachute_triggers(mock_show, example_plain_env, calisto_robust
         lag=0,
     )
 
-    _ = calisto_robust.add_parachute(
+    drogue2 = HemisphericalParachute(
         "Drogue2",
         cd_s=5.5,
         trigger=lambda pressure, height, state: height < 800 and state[5] < 0,
@@ -165,7 +165,69 @@ def test_simpler_parachute_triggers(mock_show, example_plain_env, calisto_robust
         lag=0,
     )
 
-    _ = calisto_robust.add_parachute(
+    drogue1 = HemisphericalParachute(
+        "Drogue",
+        cd_s=1.0,
+        trigger="apogee",
+        sampling_rate=105,
+        lag=0,
+    )
+    calisto_robust.add_parachute(parachute=main)
+    calisto_robust.add_parachute(parachute=drogue1)
+    calisto_robust.add_parachute(parachute=drogue2)
+
+    test_flight = Flight(
+        rocket=calisto_robust,
+        environment=example_plain_env,
+        rail_length=5,
+        inclination=85,
+        heading=0,
+    )
+
+    assert (
+        abs(test_flight.z(test_flight.parachute_events[0][0]) - test_flight.apogee) <= 1
+    )
+    assert (
+        abs(
+            test_flight.z(test_flight.parachute_events[1][0])
+            - (800 + example_plain_env.elevation)
+        )
+        <= 1
+    )
+    assert (
+        abs(
+            test_flight.z(test_flight.parachute_events[2][0])
+            - (400 + example_plain_env.elevation)
+        )
+        <= 1
+    )
+    assert calisto_robust.all_info() is None
+    assert test_flight.all_info() is None
+
+
+# TODO: When the legacy behavior is removed, remove this test
+@patch("matplotlib.pyplot.show")
+def test_legacy_add_parachute(mock_show, example_plain_env, calisto_robust):  # pylint: disable=unused-argument
+    """This is a legacy test that repeats the tests in 'test_simpler_parachute_triggers'
+    but using the 'add_parachute' method with legacy inputs. The results should be the same.
+    """
+    calisto_robust.parachutes = []
+
+    calisto_robust.add_parachute(
+        "Main",
+        cd_s=10.0,
+        trigger=400,
+        sampling_rate=105,
+        lag=0,
+    )
+    calisto_robust.add_parachute(
+        "Drogue2",
+        cd_s=5.5,
+        trigger=lambda pressure, height, state: height < 800 and state[5] < 0,
+        sampling_rate=105,
+        lag=0,
+    )
+    calisto_robust.add_parachute(
         "Drogue",
         cd_s=1.0,
         trigger="apogee",
@@ -811,3 +873,149 @@ def test_environment_methods_accessible_in_controller(
 
     # Verify all environment methods were successfully called
     assert all(methods_called.values()), f"Not all methods called: {methods_called}"
+
+
+def test_continuous_controller_invoked_every_step(calisto_robust, example_plain_env):
+    """A continuous controller (sampling_rate=None) must be called on every
+    solver step and receive the same state_history layout as a discrete one:
+    time-prefixed rows (`[t, *state]`), one element longer than ``state``.
+    This locks in the discrete/continuous parity contract."""
+    calls = {"count": 0, "sampling_rates": set(), "row_len_matches": True}
+
+    def recording_controller(  # pylint: disable=unused-argument
+        time, sampling_rate, state, state_history, observed_variables, air_brakes
+    ):
+        calls["count"] += 1
+        calls["sampling_rates"].add(sampling_rate)
+        # state_history rows are time-prefixed: exactly one longer than state
+        if len(state_history[-1]) != len(state) + 1:
+            calls["row_len_matches"] = False
+
+    calisto_robust.parachutes = []
+    calisto_robust.add_air_brakes(
+        drag_coefficient_curve="data/rockets/calisto/air_brakes_cd.csv",
+        controller_function=recording_controller,
+        sampling_rate=None,  # continuous
+        clamp=True,
+    )
+
+    flight = Flight(
+        rocket=calisto_robust,
+        environment=example_plain_env,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+        time_overshoot=False,
+        terminate_on_apogee=True,
+    )
+
+    assert flight.t_final > 0
+    # Called many times (once per solver step), far more than any fixed rate
+    assert calls["count"] > 50
+    # The controller always saw sampling_rate=None (continuous)
+    assert calls["sampling_rates"] == {None}
+    # And time-prefixed rows, consistent with the discrete controller path
+    assert calls["row_len_matches"]
+
+
+def test_discrete_controller_invoked_once_per_node(calisto_robust, example_plain_env):
+    """Regression for PR #949 (remove duplicate controller process).
+
+    A discrete controller must be invoked exactly once per time node. The
+    removed duplicate loop invoked it a second time back-to-back with the
+    identical simulation time, so no consecutive controller call may share the
+    same time value.
+    """
+    times = []
+
+    def recording_controller(  # pylint: disable=unused-argument
+        time, sampling_rate, state, state_history, observed_variables, air_brakes
+    ):
+        times.append(time)
+
+    calisto_robust.parachutes = []
+    calisto_robust.add_air_brakes(
+        drag_coefficient_curve="data/rockets/calisto/air_brakes_cd.csv",
+        controller_function=recording_controller,
+        sampling_rate=10,  # discrete controller
+        clamp=True,
+    )
+
+    flight = Flight(
+        rocket=calisto_robust,
+        environment=example_plain_env,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+        time_overshoot=False,
+        terminate_on_apogee=True,
+    )
+
+    assert flight.t_final > 0
+    assert len(times) > 10
+    # The duplicate-process bug produced two consecutive calls at the same time.
+    assert all(times[i] != times[i + 1] for i in range(len(times) - 1))
+    # No node time is processed more than once over the whole flight.
+    assert len(times) == len(set(times))
+
+
+def test_acceleration_based_parachute_trigger_deploys(
+    calisto_robust, example_plain_env
+):
+    """Integration test for PR #911: a parachute whose trigger consumes the
+    acceleration vector (a 4-argument trigger with a ``u_dot`` parameter) must
+    deploy during a full flight, exercising the u_dot code path end-to-end."""
+
+    def acc_trigger(p, h, y, u_dot):  # pylint: disable=unused-argument
+        # y[5] = vertical velocity; u_dot[5] = vertical acceleration.
+        # Deploy once descending with a downward acceleration (just past apogee).
+        return y[5] < 0 and u_dot[5] < 0
+
+    calisto_robust.parachutes = []
+    chute = HemisphericalParachute(
+        name="acc_chute",
+        cd_s=10.0,
+        trigger=acc_trigger,
+        sampling_rate=100,
+        lag=0,
+    )
+    calisto_robust.add_parachute(parachute=chute)
+
+    # Do NOT terminate at apogee: the flight must descend for the trigger to fire.
+    flight = Flight(
+        rocket=calisto_robust,
+        environment=example_plain_env,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+    )
+
+    # The acceleration (u_dot) trigger path was selected for this trigger.
+    assert getattr(chute.triggerfunc, "_expects_udot", False)
+
+    # The chute deployed, and did so essentially at apogee (first downward accel).
+    assert len(flight.parachute_events) >= 1
+    deploy_time, deployed = flight.parachute_events[0]
+    assert deployed.name == "acc_chute"
+    assert abs(flight.z(deploy_time) - flight.apogee) <= 5
+
+
+def test_to_dict_populates_parachutes_info_lazily(flight_calisto_robust):
+    """Regression: parachutes_info is filled only as a side effect of the lazy
+    post-processing pass. to_dict() must trigger that pass so the per-parachute
+    drag time series is serialized even when no post-processed property was
+    accessed first (e.g. a flight without controllers saved right after running).
+    """
+    flight = flight_calisto_robust
+
+    # Not populated yet: no post-processed property has been accessed.
+    assert flight.parachutes_info == {}
+
+    data = flight.to_dict()
+
+    # to_dict must have triggered post-processing, populating the drag series.
+    assert data["parachutes_info"]
+    assert data["parachutes_info"] is flight.parachutes_info
+    for info in data["parachutes_info"].values():
+        assert info["drag"]
+        assert info["t"]
diff --git a/tests/integration/simulation/test_monte_carlo.py b/tests/integration/simulation/test_monte_carlo.py
index 4b1b82392..98af2431d 100644
--- a/tests/integration/simulation/test_monte_carlo.py
+++ b/tests/integration/simulation/test_monte_carlo.py
@@ -236,3 +236,30 @@ def invalid_data_collector(flight):
             monte_carlo_calisto.simulate(number_of_simulations=10, append=False)
     finally:
         _post_test_file_cleanup()
+
+
+@pytest.mark.slow
+def test_monte_carlo_simulate_convergence(monte_carlo_calisto):
+    """Tests the simulate_convergence method of the MonteCarlo class.
+
+    Parameters
+    ----------
+    monte_carlo_calisto : MonteCarlo
+        The MonteCarlo object, this is a pytest fixture.
+    """
+    try:
+        ci_history = monte_carlo_calisto.simulate_convergence(
+            target_attribute="apogee",
+            target_confidence=0.95,
+            tolerance=5.0,
+            max_simulations=20,
+            batch_size=5,
+            parallel=False,
+        )
+
+        assert isinstance(ci_history, list)
+        assert all(isinstance(width, float) for width in ci_history)
+        assert len(ci_history) >= 1
+        assert monte_carlo_calisto.num_of_loaded_sims <= 20
+    finally:
+        _post_test_file_cleanup()
diff --git a/tests/integration/test_encoding.py b/tests/integration/test_encoding.py
index 38d5aef41..dc3be3432 100644
--- a/tests/integration/test_encoding.py
+++ b/tests/integration/test_encoding.py
@@ -273,10 +273,49 @@ def test_trapezoidal_fins_encoder(fin_name, request):
     assert np.isclose(fin_to_encode.tip_chord, fin_loaded.tip_chord)
     assert np.isclose(fin_to_encode.rocket_radius, fin_loaded.rocket_radius)
     assert np.isclose(fin_to_encode.sweep_length, fin_loaded.sweep_length)
-    if fin_to_encode._sweep_angle is not None and fin_loaded._sweep_angle is not None:
+    if fin_to_encode.sweep_angle is not None and fin_loaded.sweep_angle is not None:
         assert np.isclose(fin_to_encode.sweep_angle, fin_loaded.sweep_angle)
 
 
+@pytest.mark.parametrize(
+    "fin_name",
+    [
+        "calisto_trapezoidal_fin",
+        "calisto_elliptical_fin",
+        "calisto_free_form_fin",
+    ],
+)
+@pytest.mark.parametrize("include_outputs", [False, True])
+def test_individual_fin_encoder(fin_name, include_outputs, request):
+    """Test encoding an individual fin (``TrapezoidalFin``, ``EllipticalFin``
+    or ``FreeFormFin``).
+
+    Parameters
+    ----------
+    fin_name : str
+        Name of the fin fixture to encode.
+    include_outputs : bool
+        Whether to include outputs in the encoding.
+    request : pytest.FixtureRequest
+        Pytest request object.
+    """
+    fin_to_encode = request.getfixturevalue(fin_name)
+
+    json_encoded = json.dumps(
+        fin_to_encode, cls=RocketPyEncoder, include_outputs=include_outputs
+    )
+
+    fin_loaded = json.loads(json_encoded, cls=RocketPyDecoder)
+
+    assert isinstance(fin_loaded, type(fin_to_encode))
+    assert np.isclose(fin_to_encode.angular_position, fin_loaded.angular_position)
+    assert np.isclose(fin_to_encode.span, fin_loaded.span)
+    assert np.isclose(fin_to_encode.root_chord, fin_loaded.root_chord)
+    assert np.isclose(fin_to_encode.rocket_radius, fin_loaded.rocket_radius)
+    assert np.isclose(fin_to_encode.cant_angle, fin_loaded.cant_angle)
+    assert np.allclose(fin_to_encode.cp, fin_loaded.cp)
+
+
 @pytest.mark.parametrize("rocket_name", ["calisto_robust", "calisto_hybrid_modded"])
 def test_encoder_discretize(rocket_name, request):
     """Test encoding the total mass of ``rocketpy.Rocket`` with
diff --git a/tests/integration/test_rocket.py b/tests/integration/test_rocket.py
index c47096617..e36dd933e 100644
--- a/tests/integration/test_rocket.py
+++ b/tests/integration/test_rocket.py
@@ -19,7 +19,7 @@ def test_airfoil(
     calisto.add_surfaces(calisto_tail, -1.313)
 
     test_rocket.add_trapezoidal_fins(
-        2,
+        3,
         span=0.100,
         root_chord=0.120,
         tip_chord=0.040,
@@ -28,7 +28,7 @@ def test_airfoil(
         name="NACA0012",
     )
     test_rocket.add_trapezoidal_fins(
-        2,
+        3,
         span=0.100,
         root_chord=0.120,
         tip_chord=0.040,
diff --git a/tests/integration/test_sensor.py b/tests/integration/test_sensor.py
index 07b57b61b..ca9b0c8b9 100644
--- a/tests/integration/test_sensor.py
+++ b/tests/integration/test_sensor.py
@@ -11,6 +11,7 @@
 from rocketpy.sensors.barometer import Barometer
 from rocketpy.sensors.gnss_receiver import GnssReceiver
 from rocketpy.sensors.gyroscope import Gyroscope
+from rocketpy.simulation import FlightDataExporter
 
 
 def test_sensor_on_rocket(calisto_with_sensors):
@@ -107,7 +108,9 @@ def test_export_all_sensors_data(flight_calisto_with_sensors):
         Pytest fixture for the flight of the calisto rocket with a set of ideal
         sensors.
     """
-    flight_calisto_with_sensors.export_sensor_data("test_sensor_data.json")
+    FlightDataExporter(flight_calisto_with_sensors).export_sensor_data(
+        "test_sensor_data.json"
+    )
     # read the json and parse as dict
     filename = "test_sensor_data.json"
     with open(filename, "r") as f:
@@ -160,7 +163,9 @@ def test_export_single_sensor_data(flight_calisto_with_sensors):
         Pytest fixture for the flight of the calisto rocket with a set of ideal
         sensors.
     """
-    flight_calisto_with_sensors.export_sensor_data("test_sensor_data.json", "Gyroscope")
+    FlightDataExporter(flight_calisto_with_sensors).export_sensor_data(
+        "test_sensor_data.json", "Gyroscope"
+    )
     # read the json and parse as dict
     filename = "test_sensor_data.json"
     with open(filename, "r") as f:
diff --git a/tests/unit/environment/test_environment.py b/tests/unit/environment/test_environment.py
index beb6d5ac6..d56332e27 100644
--- a/tests/unit/environment/test_environment.py
+++ b/tests/unit/environment/test_environment.py
@@ -336,8 +336,8 @@ def test_resolve_dictionary_keeps_compatible_mapping(example_plain_env):
     assert resolved is gfs_mapping
 
 
-def test_resolve_dictionary_falls_back_to_legacy_mapping(example_plain_env):
-    """Fallback to a compatible built-in mapping for legacy NOMADS-style files."""
+def test_resolve_dictionary_falls_back_to_first_compatible_mapping(example_plain_env):
+    """Fallback to the first compatible built-in mapping for legacy-style files."""
     thredds_gfs_mapping = example_plain_env._Environment__weather_model_map.get("GFS")
     dataset = _DummyDataset(
         [
@@ -356,7 +356,6 @@ def test_resolve_dictionary_falls_back_to_legacy_mapping(example_plain_env):
         thredds_gfs_mapping, dataset
     )
 
-    # Explicit legacy mappings should be preferred over unrelated model mappings.
     assert resolved == example_plain_env._Environment__weather_model_map.get(
         "GFS_LEGACY"
     )
@@ -578,9 +577,10 @@ def test_set_atmospheric_model_normalizes_shortcut_case_for_forecast(example_pla
 
     called_arguments = {}
 
-    def fake_process_forecast_reanalysis(dataset, dictionary):
+    def fake_process_forecast_reanalysis(dataset, dictionary, conversion_factor):
         called_arguments["dataset"] = dataset
         called_arguments["dictionary"] = dictionary
+        called_arguments["conversion_factr"] = conversion_factor
 
     environment.process_forecast_reanalysis = fake_process_forecast_reanalysis
 
@@ -602,3 +602,108 @@ def test_set_atmospheric_model_raises_for_unknown_model_type(example_plain_env):
     # Act / Assert
     with pytest.raises(ValueError, match="Unknown model type"):
         environment.set_atmospheric_model(type="unknown_type")
+
+
+def test_wind_heading_direction_wraparound_interpolation(example_plain_env):
+    """Test that wind heading and direction interpolation wraps around correctly
+    across the 360°/0° boundary when initialized with a 2D array.
+    """
+    # Create discrete points at 1000m and 1100m
+    # 350 deg at 1000m, 10 deg at 1100m.
+    # Midpoint should be 360 deg or 0 deg, NOT 180 deg.
+    heading_data = np.array([[1000, 350], [1100, 10]])
+    direction_data = np.array([[1000, 350], [1100, 10]])
+
+    example_plain_env._Environment__set_wind_heading_function(heading_data)
+    example_plain_env._Environment__set_wind_direction_function(direction_data)
+
+    # Evaluate at midpoint (1050m)
+    mid_heading = example_plain_env.wind_heading(1050)
+    mid_direction = example_plain_env.wind_direction(1050)
+
+    # Check that it's close to 0 or 360 (which is also 0 modulo 360)
+    assert np.isclose(mid_heading, 0.0) or np.isclose(mid_heading, 360.0)
+    assert np.isclose(mid_direction, 0.0) or np.isclose(mid_direction, 360.0)
+
+    # Also test another wrap-around case, e.g. 10 to 350
+    heading_data2 = np.array([[1000, 10], [1100, 350]])
+    example_plain_env._Environment__set_wind_heading_function(heading_data2)
+    mid_heading2 = example_plain_env.wind_heading(1050)
+    assert np.isclose(mid_heading2, 0.0) or np.isclose(mid_heading2, 360.0)
+
+
+@pytest.mark.parametrize("shortcut_name", ["AIGFS", "HRRR"])
+def test_forecast_shortcut_and_dictionary_are_case_insensitive(
+    monkeypatch, shortcut_name
+):
+    """Ensure forecast shortcuts and built-in dictionaries ignore input casing."""
+    # Arrange
+    env = Environment(date=(2026, 3, 17, 12), latitude=32.99, longitude=-106.97)
+
+    sentinel_dataset = object()
+    env._Environment__atm_type_file_to_function_map["forecast"][shortcut_name] = (
+        lambda: sentinel_dataset
+    )
+
+    captured = {}
+
+    def fake_process_forecast_reanalysis(file, dictionary, conversion_factor):
+        captured["file"] = file
+        captured["dictionary"] = dictionary
+        captured["conversion_factor"] = conversion_factor
+
+    monkeypatch.setattr(
+        env, "process_forecast_reanalysis", fake_process_forecast_reanalysis
+    )
+    monkeypatch.setattr(env, "calculate_density_profile", lambda: None)
+    monkeypatch.setattr(env, "calculate_speed_of_sound_profile", lambda: None)
+    monkeypatch.setattr(env, "calculate_dynamic_viscosity", lambda: None)
+
+    # Act
+    env.set_atmospheric_model(
+        type="forecast",
+        file=shortcut_name.lower(),
+        dictionary=shortcut_name.lower(),
+    )
+
+    # Assert
+    expected_dictionary = env._Environment__weather_model_map.get(shortcut_name)
+    assert captured["file"] is sentinel_dataset
+    assert captured["dictionary"] == expected_dictionary
+    assert env.atmospheric_model_file == shortcut_name
+    assert env.atmospheric_model_dict == expected_dictionary
+
+
+def test_weather_model_mapping_get_is_case_insensitive():
+    """Ensure built-in mapping names are resolved regardless of casing."""
+    mapping = WeatherModelMapping()
+    assert mapping.get("aigfs") == mapping.get("AIGFS")
+    assert mapping.get("ecmwf_v0") == mapping.get("ECMWF_v0")
+
+
+@pytest.mark.parametrize(
+    "model, expected_factor",
+    [
+        # NOMADS-GrADS models expose pressure on the 'lev' coordinate in hPa
+        # and MUST be scaled by 100 (regression: they were forced to factor 1).
+        ("GEFS", 100),
+        ("HIRESW", 100),
+        # THREDDS (UCAR) models expose pressure on 'isobaric' already in Pa.
+        ("GFS", 1),
+        ("NAM", 1),
+        ("RAP", 1),
+        ("HRRR", 1),
+        ("AIGFS", 1),
+    ],
+)
+def test_pressure_conversion_factor_autodetect_by_model(
+    example_plain_env, model, expected_factor
+):
+    """Regression test for the GEFS/HIRESW pressure-unit bug: NOMADS-GrADS
+    models report pressure in hPa (factor 100), THREDDS models in Pa (factor 1).
+    A wrong factor silently corrupts the whole atmospheric profile (100x)."""
+    # pylint: disable=protected-access
+    factor = example_plain_env._Environment__determine_pressure_conversion_factor(
+        None, None, model
+    )
+    assert factor == expected_factor
diff --git a/tests/unit/environment/test_environment_analysis.py b/tests/unit/environment/test_environment_analysis.py
index fb86e9c04..11205ebea 100644
--- a/tests/unit/environment/test_environment_analysis.py
+++ b/tests/unit/environment/test_environment_analysis.py
@@ -161,3 +161,37 @@ def test_animation_plots(mock_show, env_analysis):  # pylint: disable=unused-arg
         HTML,
     )
     os.remove("wind_rose.gif")  # remove the files created by the method
+
+
+@pytest.mark.slow
+def test_pressure_level_wind_profile_uses_velocity_components(env_analysis):
+    """Regression for PR #1041: the redundant per-level ``wind_heading`` and
+    ``wind_direction`` functions were removed from the pressure-level data.
+
+    The surviving wind profile is expressed through ``wind_velocity_x`` /
+    ``wind_velocity_y`` (and ``wind_speed``), from which heading/direction are
+    derivable. This guards against re-introducing the removed entries and
+    checks that the surviving API is internally consistent.
+    """
+    data = env_analysis.original_pressure_level_data
+    first_date = next(iter(data))
+    first_hour = next(iter(data[first_date]))
+    hour_data = data[first_date][first_hour]
+
+    # Removed, redundant entries must not come back.
+    assert "wind_heading" not in hour_data
+    assert "wind_direction" not in hour_data
+
+    # Surviving, non-redundant wind-profile entries.
+    assert "wind_velocity_x" in hour_data
+    assert "wind_velocity_y" in hour_data
+    assert "wind_speed" in hour_data
+
+    # wind_speed must remain derivable from the velocity components. Sample at
+    # an actual grid node so interpolation and the sqrt() commute exactly.
+    grid_heights = hour_data["wind_speed"].x_array
+    height = float(grid_heights[len(grid_heights) // 2])
+    vx = hour_data["wind_velocity_x"](height)
+    vy = hour_data["wind_velocity_y"](height)
+    speed = hour_data["wind_speed"](height)
+    assert speed == pytest.approx((vx**2 + vy**2) ** 0.5, rel=1e-6)
diff --git a/tests/unit/mathutils/test_function.py b/tests/unit/mathutils/test_function.py
index 93c439def..bc28fdc61 100644
--- a/tests/unit/mathutils/test_function.py
+++ b/tests/unit/mathutils/test_function.py
@@ -1505,3 +1505,53 @@ def test_regular_grid_invalid_source_raises(bad_source, match):
             outputs=["z"],
             interpolation="regular_grid",
         )
+
+
+def test_2d_linear_interpolation_no_nan_outside_convex_hull():
+    """Test that querying a point inside the bounding box but outside the
+    convex hull does not silently return NaN.
+
+    Regression test for https://github.com/RocketPy-Team/RocketPy/issues/926.
+    The point (0.3, 0.3) lies within the axis-aligned bounding box of the
+    data but outside the convex hull, so LinearNDInterpolator would return
+    NaN without proper hull detection.
+    """
+    data = [
+        [0.0, 0.0, 0.000],
+        [0.0, 0.1, 0.100],
+        [0.0, 0.4, 0.400],
+        [0.3, 0.2, 0.150],
+    ]
+    func = Function(data, interpolation="linear")
+    result = func(0.3, 0.3)
+
+    assert not np.isnan(result), (
+        "f(0.3, 0.3) returned NaN. Point is outside the convex hull and "
+        "should be routed to extrapolation, not silently return NaN."
+    )
+
+
+def test_3d_linear_interpolation_no_nan_outside_convex_hull():
+    """Extend the convex-hull regression (issue #926) to three dimensions.
+
+    The fix in PR #969 targets N-dimensional linear interpolation, so a point
+    inside the axis-aligned bounding box but outside the convex hull must not
+    silently return NaN for 3D data either.
+    """
+    # Tetrahedron-like point cloud in the [0, 1]^3 bounding box.
+    data = [
+        [0.0, 0.0, 0.0, 0.0],
+        [1.0, 0.0, 0.0, 1.0],
+        [0.0, 1.0, 0.0, 1.0],
+        [0.0, 0.0, 1.0, 1.0],
+        [0.2, 0.2, 0.2, 0.6],
+    ]
+    func = Function(data, interpolation="linear")
+    # (0.9, 0.9, 0.9) is inside the bounding box but far outside the hull
+    # (its coordinates sum to 2.7, well beyond the x + y + z <= 1 face).
+    result = func(0.9, 0.9, 0.9)
+
+    assert not np.isnan(result), (
+        "f(0.9, 0.9, 0.9) returned NaN. Point is outside the 3D convex hull "
+        "and should be routed to extrapolation, not silently return NaN."
+    )
diff --git a/tests/unit/motors/test_genericmotor.py b/tests/unit/motors/test_genericmotor.py
index 7387189fb..7b4ff219b 100644
--- a/tests/unit/motors/test_genericmotor.py
+++ b/tests/unit/motors/test_genericmotor.py
@@ -440,3 +440,35 @@ def mock_read_fail(self, *args, **kwargs):
 
     with pytest.warns(UserWarning, match="Failed to read cached motor file"):
         GenericMotor.load_from_thrustcurve_api("M1670")
+
+
+def test_thrustcurve_api_requests_pass_timeout(monkeypatch, tmp_path):
+    """Regression for PR #940: every ThrustCurve API request must pass an
+    explicit (connect, read) timeout so the call cannot hang indefinitely."""
+    eng_path = "data/motors/cesaroni/Cesaroni_M1670.eng"
+    with open(eng_path, "rb") as f:
+        encoded = base64.b64encode(f.read()).decode("utf-8")
+
+    search_json = {"results": [{"motorId": "12345"}]}
+    download_json = {"results": [{"data": encoded}]}
+
+    captured_timeouts = []
+
+    def _capturing_get(url, **kwargs):
+        captured_timeouts.append(kwargs.get("timeout"))
+        if "search.json" in url:
+            return MockResponse(search_json)
+        if "download.json" in url:
+            return MockResponse(download_json)
+        raise RuntimeError(f"Unexpected URL: {url}")
+
+    monkeypatch.setattr(requests, "get", _capturing_get)
+    monkeypatch.setattr("rocketpy.motors.motor.CACHE_DIR", tmp_path)
+
+    GenericMotor.load_from_thrustcurve_api("M1670", no_cache=True)
+
+    assert captured_timeouts, "requests.get was never called"
+    assert all(t == (5, 30) for t in captured_timeouts), (
+        "Every ThrustCurve API request must use a (connect, read) timeout of "
+        f"(5, 30); captured timeouts were {captured_timeouts}"
+    )
diff --git a/tests/unit/motors/test_tank_geometry.py b/tests/unit/motors/test_tank_geometry.py
index ff4a525ba..e1926a7ee 100644
--- a/tests/unit/motors/test_tank_geometry.py
+++ b/tests/unit/motors/test_tank_geometry.py
@@ -1,9 +1,12 @@
+import warnings
 from pathlib import Path
 from unittest.mock import patch
 
 import numpy as np
 import pytest
 
+from rocketpy import CylindricalTank, SphericalTank
+from rocketpy.mathutils.function import Function
 from rocketpy.motors import TankGeometry
 
 PRESSURANT_PARAMS = (0.135 / 2, 0.981)
@@ -132,3 +135,127 @@ def test_tank_inertia(params, request):
 @patch("matplotlib.pyplot.show")
 def test_tank_geometry_plots_info(mock_show):  # pylint: disable=unused-argument
     assert TankGeometry({(0, 5): 1}).plots.all() is None
+
+
+def test_cylindrical_tank_radius_function_attribute():
+    """Test that CylindricalTank stores the input radius as 'radius_function'
+    and that it does not conflict with the 'radius' property (a Function of
+    height).
+    """
+    r = 0.1
+    tank = CylindricalTank(r, 2.0)
+
+    # radius_function stores the raw input scalar
+    assert tank.radius_function == r
+    # radius property is a callable Function, not the scalar
+    assert callable(tank.radius)
+    assert isinstance(tank.radius, Function)
+    # The two must differ in type
+    assert not isinstance(tank.radius_function, Function)
+
+
+def test_spherical_tank_radius_function_attribute():
+    """Test that SphericalTank stores the input radius as 'radius_function'
+    and that it does not conflict with the 'radius' property (a Function of
+    height).
+    """
+    r = 0.05
+    tank = SphericalTank(r)
+
+    # radius_function stores the raw input scalar
+    assert tank.radius_function == r
+    # radius property is a callable Function, not the scalar
+    assert callable(tank.radius)
+    assert isinstance(tank.radius, Function)
+    # The two must differ in type
+    assert not isinstance(tank.radius_function, Function)
+
+
+def test_cylindrical_tank_deprecated_radius_kwarg():
+    """Test that CylindricalTank issues a DeprecationWarning when the old
+    'radius' keyword argument is used, and still works correctly.
+    """
+    r = 0.1
+    with warnings.catch_warnings(record=True) as w:
+        warnings.simplefilter("always")
+        tank = CylindricalTank(radius=r, height=2.0)
+        assert len(w) == 1
+        assert issubclass(w[0].category, DeprecationWarning)
+        assert "radius_function" in str(w[0].message)
+
+    assert tank.radius_function == r
+
+
+def test_spherical_tank_deprecated_radius_kwarg():
+    """Test that SphericalTank issues a DeprecationWarning when the old
+    'radius' keyword argument is used, and still works correctly.
+    """
+    r = 0.05
+    with warnings.catch_warnings(record=True) as w:
+        warnings.simplefilter("always")
+        tank = SphericalTank(radius=r)
+        assert len(w) == 1
+        assert issubclass(w[0].category, DeprecationWarning)
+        assert "radius_function" in str(w[0].message)
+
+    assert tank.radius_function == r
+
+
+def test_cylindrical_tank_rejects_unknown_kwargs():
+    """The deprecated-radius **kwargs handling must not silently swallow other
+    (e.g. misspelled) keyword arguments."""
+    with pytest.raises(TypeError, match="unexpected keyword"):
+        CylindricalTank(radius_function=0.1, height=2.0, spherical_cap=True)
+
+
+def test_spherical_tank_rejects_unknown_kwargs():
+    """The deprecated-radius **kwargs handling must not silently swallow other
+    (e.g. misspelled) keyword arguments."""
+    with pytest.raises(TypeError, match="unexpected keyword"):
+        SphericalTank(radius_function=0.05, geometry_dicti={})
+
+
+def test_cylindrical_tank_to_dict_uses_radius_function_key():
+    """Test that CylindricalTank.to_dict() uses the 'radius_function' key."""
+    tank = CylindricalTank(0.1, 2.0)
+    data = tank.to_dict()
+    assert "radius_function" in data
+    assert "radius" not in data
+    assert data["radius_function"] == 0.1
+
+
+def test_spherical_tank_to_dict_uses_radius_function_key():
+    """Test that SphericalTank.to_dict() uses the 'radius_function' key."""
+    tank = SphericalTank(0.05)
+    data = tank.to_dict()
+    assert "radius_function" in data
+    assert "radius" not in data
+    assert data["radius_function"] == 0.05
+
+
+def test_cylindrical_tank_from_dict_deprecated_radius_key():
+    """Test that CylindricalTank.from_dict() issues a DeprecationWarning when
+    the serialized data contains the old 'radius' key.
+    """
+    old_data = {"radius": 0.1, "height": 2.0, "spherical_caps": False}
+    with warnings.catch_warnings(record=True) as w:
+        warnings.simplefilter("always")
+        tank = CylindricalTank.from_dict(old_data)
+        assert len(w) == 1
+        assert issubclass(w[0].category, DeprecationWarning)
+
+    assert tank.radius_function == 0.1
+
+
+def test_spherical_tank_from_dict_deprecated_radius_key():
+    """Test that SphericalTank.from_dict() issues a DeprecationWarning when
+    the serialized data contains the old 'radius' key.
+    """
+    old_data = {"radius": 0.05}
+    with warnings.catch_warnings(record=True) as w:
+        warnings.simplefilter("always")
+        tank = SphericalTank.from_dict(old_data)
+        assert len(w) == 1
+        assert issubclass(w[0].category, DeprecationWarning)
+
+    assert tank.radius_function == 0.05
diff --git a/tests/unit/rocket/aero_surface/test_fin_geometry.py b/tests/unit/rocket/aero_surface/test_fin_geometry.py
new file mode 100644
index 000000000..e4737bc40
--- /dev/null
+++ b/tests/unit/rocket/aero_surface/test_fin_geometry.py
@@ -0,0 +1,383 @@
+"""Unit tests for fin geometry strategy classes."""
+
+import numpy as np
+import pytest
+
+from rocketpy.rocket.aero_surface.fins import TrapezoidalFin, TrapezoidalFins
+from rocketpy.rocket.aero_surface.fins._geometry import (
+    _EllipticalGeometry,
+    _FreeFormGeometry,
+    _TrapezoidalGeometry,
+)
+
+
+def _make_trapezoidal_fins(cant_angle=0, n=4):
+    return TrapezoidalFins(
+        n=n,
+        root_chord=0.12,
+        tip_chord=0.04,
+        span=0.10,
+        rocket_radius=0.0635,
+        cant_angle=cant_angle,
+    )
+
+
+@pytest.mark.parametrize("cant", [3, -5, 0.5])
+def test_plural_fins_cant_angle_not_negated(cant):
+    """Regression: ``Fins.__init__`` used to store ``cant_angle`` negated, which
+    inverted the public attribute and flipped the cant-driven roll direction."""
+    fins = _make_trapezoidal_fins(cant_angle=cant)
+    assert fins.cant_angle == cant
+    np.testing.assert_allclose(fins.cant_angle_rad, np.radians(cant))
+
+
+def test_plural_fins_cant_roundtrip():
+    """``to_dict``/``from_dict`` must preserve the cant sign (it was double-
+    negated, so a save/load cycle flipped the physical cant)."""
+    fins = _make_trapezoidal_fins(cant_angle=5)
+    restored = TrapezoidalFins.from_dict(fins.to_dict())
+    assert restored.cant_angle == fins.cant_angle
+    np.testing.assert_allclose(restored.cant_angle_rad, fins.cant_angle_rad)
+
+
+def test_plural_fins_cant_setter_getter_consistency():
+    """Building with ``cant_angle=x`` and assigning ``cant_angle = x`` must yield
+    the same internal radian representation (constructor used to negate, setter
+    did not)."""
+    built = _make_trapezoidal_fins(cant_angle=5)
+    reset = _make_trapezoidal_fins(cant_angle=0)
+    reset.cant_angle = 5
+    np.testing.assert_allclose(built.cant_angle_rad, reset.cant_angle_rad)
+
+
+def test_singular_and_plural_cant_sign_parity():
+    """A single ``Fin`` and a plural ``Fins`` built with the same cant must agree
+    in ``cant_angle_rad`` (they diverged in sign when ``Fins`` negated it)."""
+    plural = _make_trapezoidal_fins(cant_angle=5)
+    single = TrapezoidalFin(
+        angular_position=0,
+        root_chord=0.12,
+        tip_chord=0.04,
+        span=0.10,
+        rocket_radius=0.0635,
+        cant_angle=5,
+    )
+    np.testing.assert_allclose(plural.cant_angle_rad, single.cant_angle_rad)
+
+
+def test_plural_fins_roll_forcing_scales_with_n():
+    """The roll forcing coefficient derivative must scale linearly with ``n``
+    (regression: it was changed to scale with ``fin_num_correction(n)``, which
+    ~halved the cant-driven roll authority for a 4-fin set)."""
+    fins4 = _make_trapezoidal_fins(cant_angle=2, n=4)
+    fins8 = _make_trapezoidal_fins(cant_angle=2, n=8)
+    clf4 = fins4.roll_parameters[0].get_value_opt(0.3)
+    clf8 = fins8.roll_parameters[0].get_value_opt(0.3)
+    np.testing.assert_allclose(clf8 / clf4, 8 / 4, rtol=1e-6)
+
+
+def test_trapezoidal_geometry_evaluate_geometrical_parameters(
+    calisto_trapezoidal_fin,
+):
+    """Ensure trapezoidal geometry populates the derived fin parameters."""
+    # Arrange
+    geometry = calisto_trapezoidal_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+
+    # Assert
+    owner = calisto_trapezoidal_fin
+    expected_area = (owner.root_chord + owner.tip_chord) * owner.span / 2
+    expected_aspect_ratio = 2 * owner.span**2 / expected_area
+    expected_gamma_c = np.arctan(
+        (geometry.sweep_length + 0.5 * owner.tip_chord - 0.5 * owner.root_chord)
+        / owner.span
+    )
+    expected_mid_aerodynamic_span = (
+        owner.span
+        / 3
+        * (owner.root_chord + 2 * owner.tip_chord)
+        / (owner.root_chord + owner.tip_chord)
+    )
+    tau = (owner.span + owner.rocket_radius) / owner.rocket_radius
+    lambda_ = owner.tip_chord / owner.root_chord
+    expected_roll_constant = (
+        (owner.root_chord + 3 * owner.tip_chord) * owner.span**3
+        + 4
+        * (owner.root_chord + 2 * owner.tip_chord)
+        * owner.rocket_radius
+        * owner.span**2
+        + 6 * (owner.root_chord + owner.tip_chord) * owner.span * owner.rocket_radius**2
+    ) / 12
+    expected_lift_interference_factor = 1 + 1 / tau
+    expected_roll_damping_factor = 1 + (
+        ((tau - lambda_) / tau) - ((1 - lambda_) / (tau - 1)) * np.log(tau)
+    ) / (
+        ((tau + 1) * (tau - lambda_)) / 2
+        - ((1 - lambda_) * (tau**3 - 1)) / (3 * (tau - 1))
+    )
+    expected_roll_forcing_factor = (1 / np.pi**2) * (
+        (np.pi**2 / 4) * ((tau + 1) ** 2 / tau**2)
+        + (np.pi * (tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+        * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+        - (2 * np.pi * (tau + 1)) / (tau * (tau - 1))
+        + ((tau**2 + 1) ** 2 / (tau**2 * (tau - 1) ** 2))
+        * (np.arcsin((tau**2 - 1) / (tau**2 + 1))) ** 2
+        - (4 * (tau + 1)) / (tau * (tau - 1)) * np.arcsin((tau**2 - 1) / (tau**2 + 1))
+        + (8 / (tau - 1) ** 2) * np.log((tau**2 + 1) / (2 * tau))
+    )
+
+    assert isinstance(geometry, _TrapezoidalGeometry)
+    assert owner.Af == pytest.approx(expected_area)
+    assert owner.AR == pytest.approx(expected_aspect_ratio)
+    assert owner.gamma_c == pytest.approx(expected_gamma_c)
+    assert owner.Yma == pytest.approx(expected_mid_aerodynamic_span)
+    assert owner.roll_geometrical_constant == pytest.approx(expected_roll_constant)
+    assert owner.tau == pytest.approx(tau)
+    assert owner.lift_interference_factor == pytest.approx(
+        expected_lift_interference_factor
+    )
+    assert owner.roll_damping_interference_factor == pytest.approx(
+        expected_roll_damping_factor
+    )
+    assert owner.roll_forcing_interference_factor == pytest.approx(
+        expected_roll_forcing_factor
+    )
+
+
+def test_trapezoidal_geometry_evaluate_shape_sets_expected_points(
+    calisto_trapezoidal_fin,
+):
+    """Ensure trapezoidal geometry shape points match the configured sweep."""
+    # Arrange
+    geometry = calisto_trapezoidal_fin.geometry
+
+    # Act
+    geometry.evaluate_shape()
+
+    # Assert
+    np.testing.assert_allclose(
+        calisto_trapezoidal_fin.shape_vec[0],
+        np.array([0.0, 0.08, 0.12, 0.12]),
+    )
+    np.testing.assert_allclose(
+        calisto_trapezoidal_fin.shape_vec[1],
+        np.array([0.0, 0.1, 0.1, 0.0]),
+    )
+
+
+def test_trapezoidal_geometry_get_data_returns_inputs_and_outputs(
+    calisto_trapezoidal_fin,
+):
+    """Ensure trapezoidal geometry serialization includes optional outputs."""
+    # Arrange
+    geometry = calisto_trapezoidal_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+    data_without_outputs = geometry.get_data()
+    data_with_outputs = geometry.get_data(include_outputs=True)
+
+    # Assert
+    assert data_without_outputs["tip_chord"] == pytest.approx(
+        calisto_trapezoidal_fin.tip_chord
+    )
+    assert data_without_outputs["sweep_length"] == pytest.approx(
+        calisto_trapezoidal_fin.sweep_length
+    )
+    assert data_without_outputs["sweep_angle"] is None
+    assert set(data_with_outputs) >= {
+        "tip_chord",
+        "sweep_length",
+        "sweep_angle",
+        "shape_vec",
+        "Af",
+        "AR",
+        "gamma_c",
+        "Yma",
+        "roll_geometrical_constant",
+        "tau",
+        "lift_interference_factor",
+        "roll_damping_interference_factor",
+        "roll_forcing_interference_factor",
+    }
+    np.testing.assert_allclose(
+        data_with_outputs["shape_vec"][0], calisto_trapezoidal_fin.shape_vec[0]
+    )
+
+
+def test_elliptical_geometry_evaluate_geometrical_parameters(
+    calisto_elliptical_fin,
+):
+    """Ensure elliptical geometry populates the derived fin parameters."""
+    # Arrange
+    geometry = calisto_elliptical_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+
+    # Assert
+    owner = calisto_elliptical_fin
+    expected_area = np.pi * owner.root_chord / 2 * owner.span / 2
+    expected_aspect_ratio = 2 * owner.span**2 / expected_area
+    expected_mid_aerodynamic_span = (
+        owner.span / (3 * np.pi) * np.sqrt(9 * np.pi**2 - 64)
+    )
+    expected_roll_constant = (
+        owner.root_chord
+        * owner.span
+        * (
+            3 * np.pi * owner.span**2
+            + 32 * owner.rocket_radius * owner.span
+            + 12 * np.pi * owner.rocket_radius**2
+        )
+        / 48
+    )
+    tau = (owner.span + owner.rocket_radius) / owner.rocket_radius
+    expected_lift_interference_factor = 1 + 1 / tau
+
+    assert isinstance(geometry, _EllipticalGeometry)
+    assert owner.Af == pytest.approx(expected_area)
+    assert owner.AR == pytest.approx(expected_aspect_ratio)
+    assert owner.gamma_c == pytest.approx(0)
+    assert owner.Yma == pytest.approx(expected_mid_aerodynamic_span)
+    assert owner.roll_geometrical_constant == pytest.approx(expected_roll_constant)
+    assert owner.tau == pytest.approx(tau)
+    assert owner.lift_interference_factor == pytest.approx(
+        expected_lift_interference_factor
+    )
+    assert owner.roll_damping_interference_factor > 0
+    assert owner.roll_forcing_interference_factor > 0
+
+
+def test_elliptical_geometry_evaluate_shape_sets_expected_points(
+    calisto_elliptical_fin,
+):
+    """Ensure elliptical geometry evaluates the expected semi-ellipse shape."""
+    # Arrange
+    geometry = calisto_elliptical_fin.geometry
+
+    # Act
+    geometry.evaluate_shape()
+
+    # Assert
+    angles = np.arange(0, 180, 5)
+    expected_x = calisto_elliptical_fin.root_chord / 2 + (
+        calisto_elliptical_fin.root_chord / 2 * np.cos(np.radians(angles))
+    )
+    expected_y = calisto_elliptical_fin.span * np.sin(np.radians(angles))
+    np.testing.assert_allclose(calisto_elliptical_fin.shape_vec[0], expected_x)
+    np.testing.assert_allclose(calisto_elliptical_fin.shape_vec[1], expected_y)
+
+
+def test_elliptical_geometry_get_data_returns_expected_outputs(
+    calisto_elliptical_fin,
+):
+    """Ensure elliptical geometry serialization includes optional outputs."""
+    # Arrange
+    geometry = calisto_elliptical_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+    data_without_outputs = geometry.get_data()
+    data_with_outputs = geometry.get_data(include_outputs=True)
+
+    # Assert
+    assert data_without_outputs == {}
+    assert data_with_outputs["Af"] == pytest.approx(calisto_elliptical_fin.Af)
+    assert data_with_outputs["AR"] == pytest.approx(calisto_elliptical_fin.AR)
+    assert data_with_outputs["gamma_c"] == pytest.approx(calisto_elliptical_fin.gamma_c)
+    assert data_with_outputs["Yma"] == pytest.approx(calisto_elliptical_fin.Yma)
+    assert data_with_outputs["roll_geometrical_constant"] == pytest.approx(
+        calisto_elliptical_fin.roll_geometrical_constant
+    )
+    assert data_with_outputs["tau"] == pytest.approx(calisto_elliptical_fin.tau)
+
+
+def test_free_form_geometry_infer_dimensions_warns_on_jagged_shape():
+    """Ensure jagged free-form fins emit a warning while dimensions are inferred."""
+    # Arrange
+    shape_points = [(0, 0), (0.05, 0.1), (0.06, 0.05), (0.09, 0.07), (0.12, 0)]
+
+    # Act
+    with pytest.warns(UserWarning, match="Jagged fin shape detected"):
+        root_chord, span = _FreeFormGeometry.infer_dimensions(shape_points)
+
+    # Assert
+    assert root_chord == pytest.approx(0.12)
+    assert span == pytest.approx(0.1)
+
+
+def test_free_form_geometry_evaluate_geometrical_parameters(calisto_free_form_fin):
+    """Ensure free-form geometry populates the derived fin parameters."""
+    # Arrange
+    geometry = calisto_free_form_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+
+    # Assert
+    owner = calisto_free_form_fin
+    assert isinstance(geometry, _FreeFormGeometry)
+    assert owner.Af == pytest.approx(0.008)
+    assert owner.AR == pytest.approx(2.5)
+    assert owner.gamma_c > 0
+    assert owner.Yma > 0
+    assert owner.mac_length > 0
+    assert owner.mac_lead >= 0
+    assert owner.roll_geometrical_constant > 0
+    assert owner.tau > 0
+    assert owner.lift_interference_factor > 1
+    assert owner.roll_damping_interference_factor > 1
+    assert owner.roll_forcing_interference_factor > 0
+
+
+def test_free_form_geometry_evaluate_shape_sets_expected_points(
+    calisto_free_form_fin,
+):
+    """Ensure free-form geometry exposes the configured shape points."""
+    # Arrange
+    geometry = calisto_free_form_fin.geometry
+
+    # Act
+    geometry.evaluate_shape()
+
+    # Assert
+    np.testing.assert_allclose(
+        calisto_free_form_fin.shape_vec[0],
+        np.array([0.0, 0.08, 0.12, 0.12]),
+    )
+    np.testing.assert_allclose(
+        calisto_free_form_fin.shape_vec[1],
+        np.array([0.0, 0.1, 0.1, 0.0]),
+    )
+
+
+def test_free_form_geometry_get_data_returns_expected_outputs(
+    calisto_free_form_fin,
+):
+    """Ensure free-form geometry serialization includes optional outputs."""
+    # Arrange
+    geometry = calisto_free_form_fin.geometry
+
+    # Act
+    geometry.evaluate_geometrical_parameters()
+    data_without_outputs = geometry.get_data()
+    data_with_outputs = geometry.get_data(include_outputs=True)
+
+    # Assert
+    assert data_without_outputs == {
+        "shape_points": [(0, 0), (0.08, 0.1), (0.12, 0.1), (0.12, 0)],
+    }
+    assert data_with_outputs["shape_points"] == calisto_free_form_fin.shape_points
+    assert data_with_outputs["Af"] == pytest.approx(calisto_free_form_fin.Af)
+    assert data_with_outputs["AR"] == pytest.approx(calisto_free_form_fin.AR)
+    assert data_with_outputs["gamma_c"] == pytest.approx(calisto_free_form_fin.gamma_c)
+    assert data_with_outputs["Yma"] == pytest.approx(calisto_free_form_fin.Yma)
+    assert data_with_outputs["mac_length"] == pytest.approx(
+        calisto_free_form_fin.mac_length
+    )
+    assert data_with_outputs["mac_lead"] == pytest.approx(
+        calisto_free_form_fin.mac_lead
+    )
diff --git a/tests/unit/rocket/aero_surface/test_individual_fins.py b/tests/unit/rocket/aero_surface/test_individual_fins.py
new file mode 100644
index 000000000..f30bb52cc
--- /dev/null
+++ b/tests/unit/rocket/aero_surface/test_individual_fins.py
@@ -0,0 +1,460 @@
+"""Unit tests for individual fin classes."""
+
+from unittest.mock import patch
+
+import numpy as np
+import pytest
+
+from rocketpy import (
+    EllipticalFin,
+    FreeFormFin,
+    Rocket,
+    TrapezoidalFin,
+    TrapezoidalFins,
+)
+from rocketpy.mathutils.vector_matrix import Vector
+
+
+@pytest.mark.parametrize(
+    "fixture_name,expected_class",
+    [
+        ("calisto_trapezoidal_fin", TrapezoidalFin),
+        ("calisto_elliptical_fin", EllipticalFin),
+        ("calisto_free_form_fin", FreeFormFin),
+    ],
+)
+def test_individual_fin_info_returns_none(request, fixture_name, expected_class):
+    """Ensure info() executes for all individual fin classes."""
+    # Arrange
+    fin = request.getfixturevalue(fixture_name)
+
+    # Act
+    result = fin.info()
+
+    # Assert
+    assert isinstance(fin, expected_class)
+    assert result is None
+
+
+@patch("matplotlib.pyplot.show")
+@pytest.mark.parametrize(
+    "fixture_name",
+    [
+        "calisto_trapezoidal_fin",
+        "calisto_elliptical_fin",
+        "calisto_free_form_fin",
+    ],
+)
+def test_individual_fin_draw_returns_none(mock_show, request, fixture_name):  # pylint: disable=unused-argument
+    """Ensure draw() executes for all individual fin classes."""
+    # Arrange
+    fin = request.getfixturevalue(fixture_name)
+
+    # Act
+    result = fin.draw(filename=None)
+
+    # Assert
+    assert result is None
+
+
+@pytest.mark.parametrize(
+    "fixture_name",
+    [
+        "calisto_trapezoidal_fin",
+        "calisto_elliptical_fin",
+        "calisto_free_form_fin",
+    ],
+)
+def test_individual_fin_angular_position_updates_radians(request, fixture_name):
+    """Ensure angular_position setter updates angular_position_rad."""
+    # Arrange
+    fin = request.getfixturevalue(fixture_name)
+
+    # Act
+    fin.angular_position = 45
+
+    # Assert
+    assert fin.angular_position == 45
+    np.testing.assert_allclose(fin.angular_position_rad, np.pi / 4)
+
+
+def test_trapezoidal_fin_setters_update_geometry(calisto_trapezoidal_fin):
+    """Ensure trapezoidal fin geometry setters update exposed values."""
+    # Arrange
+    fin = calisto_trapezoidal_fin
+
+    # Act
+    fin.tip_chord = 0.05
+    fin.sweep_angle = 12.0
+    fin.sweep_length = 0.03
+
+    # Assert
+    np.testing.assert_allclose(fin.tip_chord, 0.05)
+    np.testing.assert_allclose(fin.sweep_angle, 12.0)
+    np.testing.assert_allclose(fin.sweep_length, 0.03)
+
+
+def test_individual_fin_rocket_diameter_aliases_are_kept_in_sync(
+    calisto_trapezoidal_fin,
+):
+    """Ensure rocket_diameter is canonical and old aliases remain compatible."""
+    # Arrange
+    fin = calisto_trapezoidal_fin
+
+    # Act
+    fin.rocket_diameter = 0.15
+
+    # Assert
+    np.testing.assert_allclose(fin.rocket_diameter, 0.15)
+    np.testing.assert_allclose(fin.diameter, 0.15)
+    np.testing.assert_allclose(fin.d, 0.15)
+    np.testing.assert_allclose(fin.rocket_radius, 0.075)
+    np.testing.assert_allclose(fin.reference_length, 0.15)
+
+    # Act
+    fin.d = 0.20
+
+    # Assert
+    np.testing.assert_allclose(fin.rocket_diameter, 0.20)
+    np.testing.assert_allclose(fin.diameter, 0.20)
+    np.testing.assert_allclose(fin.d, 0.20)
+    np.testing.assert_allclose(fin.rocket_radius, 0.10)
+    np.testing.assert_allclose(fin.reference_length, 0.20)
+
+
+def test_individual_fin_reference_area_and_ref_area_alias_are_kept_in_sync(
+    calisto_trapezoidal_fin,
+):
+    """Ensure reference_area is canonical and ref_area remains compatible."""
+    # Arrange
+    fin = calisto_trapezoidal_fin
+
+    # Act
+    fin.reference_area = 0.123
+
+    # Assert
+    np.testing.assert_allclose(fin.reference_area, 0.123)
+    np.testing.assert_allclose(fin.ref_area, 0.123)
+
+    # Act
+    fin.ref_area = 0.456
+
+    # Assert
+    np.testing.assert_allclose(fin.reference_area, 0.456)
+    np.testing.assert_allclose(fin.ref_area, 0.456)
+
+
+def test_individual_fin_to_dict_include_outputs_exposes_diameter_aliases(
+    calisto_trapezoidal_fin,
+):
+    """Ensure output serialization exposes canonical and alias diameter keys."""
+    # Arrange
+    fin = calisto_trapezoidal_fin
+
+    # Act
+    data = fin.to_dict(include_outputs=True)
+
+    # Assert
+    np.testing.assert_allclose(data["rocket_diameter"], fin.rocket_diameter)
+    np.testing.assert_allclose(data["diameter"], fin.rocket_diameter)
+    np.testing.assert_allclose(data["d"], fin.rocket_diameter)
+    np.testing.assert_allclose(data["reference_area"], fin.reference_area)
+    np.testing.assert_allclose(data["ref_area"], fin.reference_area)
+
+
+def test_trapezoidal_fin_rejects_inconsistent_sweep_inputs():
+    """Ensure trapezoidal fin rejects sweep_length with sweep_angle together."""
+    # Arrange / Act / Assert
+    with pytest.raises(
+        ValueError, match="Cannot use sweep_length and sweep_angle together"
+    ):
+        TrapezoidalFin(
+            angular_position=0,
+            root_chord=0.12,
+            tip_chord=0.04,
+            span=0.1,
+            rocket_radius=0.0635,
+            sweep_length=0.02,
+            sweep_angle=10.0,
+        )
+
+
+def test_free_form_fin_shape_points_property(calisto_free_form_fin):
+    """Ensure free-form fin exposes the original shape points."""
+    # Arrange
+    fin = calisto_free_form_fin
+
+    # Act
+    shape_points = fin.shape_points
+
+    # Assert
+    assert shape_points == [(0, 0), (0.08, 0.1), (0.12, 0.1), (0.12, 0)]
+
+
+@pytest.mark.parametrize(
+    "fixture_name,required_keys",
+    [
+        (
+            "calisto_trapezoidal_fin",
+            {
+                "angular_position",
+                "root_chord",
+                "span",
+                "rocket_radius",
+                "cant_angle",
+                "airfoil",
+                "name",
+                "tip_chord",
+                "sweep_length",
+                "sweep_angle",
+            },
+        ),
+        (
+            "calisto_elliptical_fin",
+            {
+                "angular_position",
+                "root_chord",
+                "span",
+                "rocket_radius",
+                "cant_angle",
+                "airfoil",
+                "name",
+            },
+        ),
+        (
+            "calisto_free_form_fin",
+            {
+                "angular_position",
+                "rocket_radius",
+                "cant_angle",
+                "airfoil",
+                "name",
+                "shape_points",
+            },
+        ),
+    ],
+)
+def test_individual_fin_to_dict_contains_expected_keys(
+    request, fixture_name, required_keys
+):
+    """Ensure to_dict for each individual fin exposes expected input keys."""
+    # Arrange
+    fin = request.getfixturevalue(fixture_name)
+
+    # Act
+    data = fin.to_dict()
+
+    # Assert
+    assert required_keys.issubset(data.keys())
+
+
+@pytest.mark.parametrize(
+    "fixture_name,fin_class,comparisons",
+    [
+        (
+            "calisto_trapezoidal_fin",
+            TrapezoidalFin,
+            ["angular_position", "root_chord", "tip_chord", "span", "rocket_radius"],
+        ),
+        (
+            "calisto_elliptical_fin",
+            EllipticalFin,
+            ["angular_position", "root_chord", "span", "rocket_radius"],
+        ),
+        (
+            "calisto_free_form_fin",
+            FreeFormFin,
+            ["angular_position", "rocket_radius"],
+        ),
+    ],
+)
+def test_individual_fin_from_dict_roundtrip(
+    request, fixture_name, fin_class, comparisons
+):
+    """Ensure each individual fin can be reconstructed with from_dict."""
+    # Arrange
+    fin = request.getfixturevalue(fixture_name)
+    data = fin.to_dict()
+
+    # Act
+    reconstructed = fin_class.from_dict(data)
+
+    # Assert
+    assert isinstance(reconstructed, fin_class)
+    for field in comparisons:
+        np.testing.assert_allclose(getattr(reconstructed, field), getattr(fin, field))
+
+    if fin_class is FreeFormFin:
+        assert reconstructed.shape_points == fin.shape_points
+
+
+def test_trapezoidal_fin_from_dict_roundtrip_preserves_sweep_length():
+    """Ensure TrapezoidalFin round-trip preserves non-default sweep geometry."""
+    # Arrange
+    original = TrapezoidalFin(
+        angular_position=0,
+        root_chord=0.12,
+        tip_chord=0.04,
+        span=0.1,
+        rocket_radius=0.0635,
+        cant_angle=0,
+        sweep_angle=15.0,
+        name="roundtrip_trapezoidal_fin",
+    )
+    data = original.to_dict()
+
+    # Act
+    reconstructed = TrapezoidalFin.from_dict(data)
+
+    # Assert
+    np.testing.assert_allclose(reconstructed.sweep_length, original.sweep_length)
+
+
+def test_calisto_finset_vs_four_individual_fins_close():
+    """Ensure a 4-fin set and 4 individual fins produce close aerodynamics.
+
+    Notes
+    -----
+    A fin set model includes finite-set lift correction for the number of fins.
+    For 4 fins, this correction is equivalent to scaling the sum of 4
+    individual-fin lift derivatives by 1/2.
+    """
+    # Arrange
+    finset_rocket = Rocket(
+        radius=0.0635,
+        mass=14.426,
+        inertia=(6.321, 6.321, 0.034),
+        power_off_drag="data/rockets/calisto/powerOffDragCurve.csv",
+        power_on_drag="data/rockets/calisto/powerOnDragCurve.csv",
+        center_of_mass_without_motor=0,
+        coordinate_system_orientation="tail_to_nose",
+    )
+    finset_rocket.add_surfaces(
+        TrapezoidalFins(
+            n=4,
+            span=0.100,
+            root_chord=0.120,
+            tip_chord=0.040,
+            rocket_radius=0.0635,
+            name="calisto_trapezoidal_fins",
+            cant_angle=0,
+            sweep_length=None,
+            sweep_angle=None,
+            airfoil=None,
+        ),
+        -1.168,
+    )
+
+    individual_fins_rocket = Rocket(
+        radius=0.0635,
+        mass=14.426,
+        inertia=(6.321, 6.321, 0.034),
+        power_off_drag="data/rockets/calisto/powerOffDragCurve.csv",
+        power_on_drag="data/rockets/calisto/powerOnDragCurve.csv",
+        center_of_mass_without_motor=0,
+        coordinate_system_orientation="tail_to_nose",
+    )
+
+    individual_fins = [
+        TrapezoidalFin(
+            angular_position=angle,
+            root_chord=0.120,
+            tip_chord=0.040,
+            span=0.100,
+            rocket_radius=0.0635,
+            name=f"calisto_trapezoidal_fin_{i}",
+            cant_angle=0,
+            sweep_length=None,
+            sweep_angle=None,
+            airfoil=None,
+        )
+        for i, angle in enumerate((0, 90, 180, 270), start=1)
+    ]
+    individual_fins_rocket.add_surfaces(individual_fins, [-1.168] * 4)
+
+    mach_grid = np.linspace(0, 2, 21)
+
+    # Act
+    cp_finset = finset_rocket.cp_position(mach_grid)
+    cp_individual = individual_fins_rocket.cp_position(mach_grid)
+    clalpha_finset = finset_rocket.total_lift_coeff_der(mach_grid)
+    clalpha_individual = individual_fins_rocket.total_lift_coeff_der(mach_grid)
+    lift_correction = TrapezoidalFins.fin_num_correction(4) / 4
+    clalpha_individual_corrected = np.array(clalpha_individual) * lift_correction
+
+    # Assert
+    np.testing.assert_allclose(cp_individual, cp_finset, rtol=1e-6, atol=1e-6)
+    np.testing.assert_allclose(clalpha_individual_corrected, clalpha_finset)
+
+
+def test_individual_fin_roll_damping_not_double_counted():
+    """Regression: roll damping for an individual fin must come solely from the
+    roll-rate velocity that the Flight loop injects into the local stream
+    velocity (``w ^ cp`` at the off-axis center of pressure), captured by the
+    ``cp ^ R`` moment. An extra explicit ``cld_omega * omega3`` term used to be
+    added on top, double-counting the damping. The roll moment must therefore be
+    invariant to the explicit ``omega`` argument for a fixed stream velocity, and
+    must still respond to a tangential (roll-induced) stream component."""
+    fin = TrapezoidalFin(
+        angular_position=0,  # fin located at +y, so its CP is off the roll axis
+        root_chord=0.12,
+        tip_chord=0.04,
+        span=0.10,
+        rocket_radius=0.0635,
+        cant_angle=0,
+    )
+    cp = Vector([0.0, 0.0635, -1.0])
+    axial_stream = Vector([0.0, 0.0, 30.0])
+    tangential_stream = Vector([3.0, 0.0, 30.0])  # +x mimics roll-induced flow
+
+    def roll_moment(stream, omega3):
+        return fin.compute_forces_and_moments(
+            stream, abs(stream), 0.1, 1.2, cp, (0.0, 0.0, omega3)
+        )[5]
+
+    # The explicit omega argument must not add a separate damping term.
+    m_omega_0 = roll_moment(tangential_stream, 0.0)
+    m_omega_50 = roll_moment(tangential_stream, 50.0)
+    np.testing.assert_allclose(m_omega_0, m_omega_50, atol=1e-12)
+
+    # Damping is still produced: a tangential (roll-induced) stream component
+    # changes the roll moment relative to purely axial flow.
+    m_axial = roll_moment(axial_stream, 0.0)
+    assert abs(m_omega_0 - m_axial) > 1e-6
+
+
+@pytest.mark.parametrize(
+    "position_input",
+    [
+        (0.02, -0.01, -1.2),
+        Vector([0.02, -0.01, -1.2]),
+    ],
+)
+def test_add_individual_fin_accepts_full_3d_position(position_input):
+    """Ensure individual fins accept full (x, y, z) position inputs."""
+    # Arrange
+    rocket = Rocket(
+        radius=0.0635,
+        mass=14.426,
+        inertia=(6.321, 6.321, 0.034),
+        power_off_drag="data/rockets/calisto/powerOffDragCurve.csv",
+        power_on_drag="data/rockets/calisto/powerOnDragCurve.csv",
+        center_of_mass_without_motor=0,
+        coordinate_system_orientation="tail_to_nose",
+    )
+    fin = TrapezoidalFin(
+        angular_position=30,
+        root_chord=0.120,
+        tip_chord=0.040,
+        span=0.100,
+        rocket_radius=0.0635,
+        cant_angle=0,
+        name="position_test_fin",
+    )
+
+    # Act
+    rocket.add_surfaces(fin, position_input)
+    stored_position = rocket.aerodynamic_surfaces[0].position
+
+    # Assert
+    assert stored_position == Vector([0.02, -0.01, -1.2])
diff --git a/tests/unit/rocket/test_parachute.py b/tests/unit/rocket/test_parachute.py
index e193b777b..310c85aac 100644
--- a/tests/unit/rocket/test_parachute.py
+++ b/tests/unit/rocket/test_parachute.py
@@ -4,7 +4,7 @@
 import numpy as np
 import pytest
 
-from rocketpy import Parachute
+from rocketpy import HemisphericalParachute, Parachute
 
 
 def _make_parachute(**kwargs):
@@ -15,7 +15,7 @@ def _make_parachute(**kwargs):
         "sampling_rate": 100,
     }
     defaults.update(kwargs)
-    return Parachute(**defaults)
+    return HemisphericalParachute(**defaults)
 
 
 class TestParachuteRadiusEstimation:
@@ -91,7 +91,7 @@ def test_from_dict_round_trip_preserves_drag_coefficient(self):
         drag_coefficient."""
         original = _make_parachute(cd_s=5.0, drag_coefficient=0.75)
         data = original.to_dict()
-        restored = Parachute.from_dict(data)
+        restored = HemisphericalParachute.from_dict(data)
         assert restored.drag_coefficient == pytest.approx(0.75)
         assert restored.radius == pytest.approx(original.radius, rel=1e-9)
 
@@ -107,5 +107,30 @@ def test_from_dict_defaults_drag_coefficient_to_1_4_when_absent(self):
             "noise": (0, 0, 0),
             # no drag_coefficient key — simulates old serialized data
         }
-        parachute = Parachute.from_dict(data)
+        parachute = HemisphericalParachute.from_dict(data)
         assert parachute.drag_coefficient == pytest.approx(1.4)
+
+
+class TestParachuteAbstractBase:
+    """After the PR #958 refactor, ``Parachute`` is an abstract base class and
+    users must instantiate a concrete model such as ``HemisphericalParachute``."""
+
+    def test_parachute_abstract_base_cannot_be_instantiated(self):
+        """Instantiating the abstract ``Parachute`` base directly must raise a
+        ``TypeError`` (unimplemented abstract methods)."""
+        with pytest.raises(TypeError, match="abstract"):
+            # pylint: disable=abstract-class-instantiated,unexpected-keyword-arg
+            # pylint: disable=no-value-for-parameter
+            Parachute(
+                name="test",
+                cd_s=10.0,
+                trigger="apogee",
+                sampling_rate=100,
+            )
+
+    def test_hemispherical_parachute_is_a_parachute_subclass(self):
+        """The concrete ``HemisphericalParachute`` must derive from the abstract
+        ``Parachute`` base."""
+        assert issubclass(HemisphericalParachute, Parachute)
+        parachute = _make_parachute()
+        assert isinstance(parachute, Parachute)
diff --git a/tests/unit/rocket/test_rocket.py b/tests/unit/rocket/test_rocket.py
index 3c7725fa5..18ad5680b 100644
--- a/tests/unit/rocket/test_rocket.py
+++ b/tests/unit/rocket/test_rocket.py
@@ -5,7 +5,12 @@
 import numpy as np
 import pytest
 
-from rocketpy import Function, NoseCone, Rocket, SolidMotor
+from rocketpy import Function, GenericSurface, NoseCone, Rocket, SolidMotor
+from rocketpy.exceptions import (
+    InvalidInertiaError,
+    InvalidParameterError,
+    UnstableRocketWarning,
+)
 from rocketpy.mathutils.vector_matrix import Vector
 from rocketpy.motors.empty_motor import EmptyMotor
 from rocketpy.motors.motor import Motor
@@ -835,3 +840,159 @@ def test_drag_input_types_supported_for_power_on_and_power_off(tmp_path):
 
         assert rocket.power_off_drag_7d(*query_point) == pytest.approx(expected)
         assert rocket.power_on_drag_7d(*query_point) == pytest.approx(expected)
+
+
+@pytest.mark.parametrize("radius", [-1, 0, -0.001])
+def test_rocket_invalid_radius_raises(radius):
+    """InvalidParameterError must be raised for non-positive radius values."""
+    with pytest.raises(InvalidParameterError, match="radius"):
+        Rocket(
+            radius=radius,
+            mass=10,
+            inertia=(0.1, 0.1, 0.01),
+            power_off_drag=0.3,
+            power_on_drag=0.3,
+            center_of_mass_without_motor=0,
+        )
+
+
+@pytest.mark.parametrize("mass", [-1, 0, -0.001])
+def test_rocket_invalid_mass_raises(mass):
+    """InvalidParameterError must be raised for non-positive mass values."""
+    with pytest.raises(InvalidParameterError, match="mass"):
+        Rocket(
+            radius=0.05,
+            mass=mass,
+            inertia=(0.1, 0.1, 0.01),
+            power_off_drag=0.3,
+            power_on_drag=0.3,
+            center_of_mass_without_motor=0,
+        )
+
+
+@pytest.mark.parametrize("inertia", [(0.1,), (0.1, 0.1), (0.1, 0.1, 0.01, 0.0, 0.0)])
+def test_rocket_invalid_inertia_length_raises(inertia):
+    """InvalidInertiaError must be raised when inertia tuple has wrong length."""
+    with pytest.raises(InvalidInertiaError):
+        Rocket(
+            radius=0.05,
+            mass=10,
+            inertia=inertia,
+            power_off_drag=0.3,
+            power_on_drag=0.3,
+            center_of_mass_without_motor=0,
+        )
+
+
+@pytest.mark.parametrize(
+    "inertia",
+    [
+        np.array([6.321, 6.321, 0.034]),
+        np.array([6.321, 6.321, 0.034, 0.0, 0.0, 0.0]),
+    ],
+)
+def test_rocket_accepts_numpy_inertia_and_scalars(inertia):
+    """Regression: numpy-array inertia and numpy numeric scalars for
+    radius/mass must be accepted (they were rejected by an overly strict
+    isinstance check, breaking code that computes inertia tensors with numpy)."""
+    rocket = Rocket(
+        radius=np.float64(0.05),
+        mass=np.int64(10),
+        inertia=inertia,
+        power_off_drag=0.3,
+        power_on_drag=0.3,
+        center_of_mass_without_motor=0,
+    )
+    assert rocket.I_11_without_motor == inertia[0]
+    assert rocket.I_33_without_motor == inertia[2]
+
+
+def test_add_trapezoidal_fins_two_fins_warns_but_succeeds(calisto):
+    """Regression: fin sets with n<=2 must still be accepted (as on master),
+    now with an informative warning instead of a hard error."""
+    with pytest.warns(UserWarning, match="2 or fewer fins"):
+        fins = calisto.add_trapezoidal_fins(
+            2, span=0.1, root_chord=0.12, tip_chord=0.04, position=-1.0
+        )
+    assert fins in [surface for surface, _ in calisto.aerodynamic_surfaces]
+
+
+def test_unstable_rocket_warning_raised(calisto):
+    """UnstableRocketWarning must be raised (at finalization, e.g. via
+    ``warn_if_unstable``) when the static margin at motor ignition is negative.
+    The warning must NOT fire during incremental ``add_surfaces`` construction,
+    to avoid spurious warnings for partially-built-but-stable rockets."""
+    nose = NoseCone(
+        length=0.55829,
+        kind="vonkarman",
+        base_radius=0.0635,
+        rocket_radius=0.0635,
+        name="Nose Cone",
+    )
+    # Adding surfaces during construction must not warn.
+    with warnings.catch_warnings():
+        warnings.simplefilter("error", UnstableRocketWarning)
+        calisto.add_surfaces(nose, 1.16)
+
+    # The check fires explicitly once the rocket is finalized.
+    with pytest.warns(UnstableRocketWarning):
+        calisto.warn_if_unstable()
+    assert calisto.static_margin(0) < 0
+
+
+def test_unstable_rocket_warning_skipped_with_generic_surface(calisto):
+    """UnstableRocketWarning must not be raised when the rocket has a
+    GenericSurface, since its lift coefficient derivative is not accounted
+    for in the center of pressure calculation, making the static margin
+    unreliable for this check."""
+    nose = NoseCone(
+        length=0.55829,
+        kind="vonkarman",
+        base_radius=0.0635,
+        rocket_radius=0.0635,
+        name="Nose Cone",
+    )
+    generic_surface = GenericSurface(
+        reference_area=None,
+        reference_length=None,
+        coefficients={
+            "cL": lambda alpha, beta, mach, reynolds, pitch_rate, yaw_rate, roll_rate: 1
+        },
+    )
+    with warnings.catch_warnings():
+        warnings.simplefilter("error", UnstableRocketWarning)
+        calisto.add_surfaces([nose, generic_surface], [1.16, 0])
+        calisto.warn_if_unstable()
+    assert calisto.static_margin(0) < 0
+
+
+def test_power_drag_exposed_as_function_objects_and_inputs_preserved():
+    """Regression for PR #941: ``power_off_drag``/``power_on_drag`` must be
+    exposed as Mach-only ``Function`` objects, while the raw user input is
+    preserved in the ``_power_off_drag_input``/``_power_on_drag_input``
+    attributes."""
+    off_input = "data/rockets/calisto/powerOffDragCurve.csv"
+    on_input = "data/rockets/calisto/powerOnDragCurve.csv"
+    rocket = Rocket(
+        radius=0.0635,
+        mass=14.426,
+        inertia=(6.321, 6.321, 0.034),
+        power_off_drag=off_input,
+        power_on_drag=on_input,
+        center_of_mass_without_motor=0,
+        coordinate_system_orientation="tail_to_nose",
+    )
+
+    # Public drag attributes are Function objects (Mach-only aliases).
+    assert isinstance(rocket.power_off_drag, Function)
+    assert isinstance(rocket.power_on_drag, Function)
+    assert rocket.power_off_drag(0.5) == pytest.approx(
+        rocket.power_off_drag_7d(0, 0, 0.5, 0, 0, 0, 0)
+    )
+    assert rocket.power_on_drag(0.5) == pytest.approx(
+        rocket.power_on_drag_7d(0, 0, 0.5, 0, 0, 0, 0)
+    )
+
+    # Raw user input is preserved for serialization / round-tripping.
+    assert rocket._power_off_drag_input == off_input
+    assert rocket._power_on_drag_input == on_input
diff --git a/tests/unit/sensors/test_sensor.py b/tests/unit/sensors/test_sensor.py
index 0813a3638..7273282dc 100644
--- a/tests/unit/sensors/test_sensor.py
+++ b/tests/unit/sensors/test_sensor.py
@@ -8,6 +8,16 @@
 from rocketpy.mathutils.vector_matrix import Matrix, Vector
 from rocketpy.tools import euler313_to_quaternions
 
+
+@pytest.fixture(autouse=True)
+def _seed_rng():
+    """Seed NumPy's global RNG before each test so that the noise-based
+    sensor measurements are deterministic. Without this, tests such as
+    ``test_noisy_barometer`` are flaky because the random white noise can
+    occasionally exceed the assertion tolerance."""
+    np.random.seed(42)
+
+
 # calisto standard simulation no wind solution index 200
 TIME = 3.338513236767685
 U = [
diff --git a/tests/unit/simulation/test_flight.py b/tests/unit/simulation/test_flight.py
index 9af1c5fd5..9a3c54477 100644
--- a/tests/unit/simulation/test_flight.py
+++ b/tests/unit/simulation/test_flight.py
@@ -8,6 +8,7 @@
 from scipy import optimize
 
 from rocketpy import Components, Flight, Function, Rocket
+from rocketpy.simulation import FlightDataExporter
 
 plt.rcParams.update({"figure.max_open_warning": 0})
 
@@ -174,7 +175,9 @@ def test_export_sensor_data(flight_calisto_with_sensors):
     flight_calisto_with_sensors : Flight
         Pytest fixture for the flight of the calisto rocket with an ideal accelerometer and a gyroscope.
     """
-    flight_calisto_with_sensors.export_sensor_data("test_sensor_data.json")
+    FlightDataExporter(flight_calisto_with_sensors).export_sensor_data(
+        "test_sensor_data.json"
+    )
     # read the json and parse as dict
     filename = "test_sensor_data.json"
     with open(filename, "r") as f:
diff --git a/tests/unit/simulation/test_flight_time_nodes.py b/tests/unit/simulation/test_flight_time_nodes.py
index 20769b1f8..2c330d30a 100644
--- a/tests/unit/simulation/test_flight_time_nodes.py
+++ b/tests/unit/simulation/test_flight_time_nodes.py
@@ -2,7 +2,7 @@
 TimeNode.
 """
 
-# from rocketpy.rocket import Parachute, _Controller
+from rocketpy.control.controller import _Controller
 
 
 def test_time_nodes_init(flight_calisto):
@@ -49,6 +49,32 @@ def test_time_nodes_add_node(flight_calisto):
 # TODO: implement this test
 
 
+def test_time_nodes_add_controllers_skips_continuous_controllers(flight_calisto):
+    """Ensure only discrete controllers create time nodes."""
+    # Arrange
+    discrete_controller = _Controller(
+        interactive_objects=[],
+        controller_function=lambda t, sr, sv, sh, ov, io: None,
+        sampling_rate=10,
+        name="Discrete",
+    )
+    continuous_controller = _Controller(
+        interactive_objects=[],
+        controller_function=lambda t, sr, sv, sh, ov, io: None,
+        sampling_rate=None,
+        name="Continuous",
+    )
+    time_nodes = flight_calisto.TimeNodes()
+
+    # Act
+    time_nodes.add_controllers([discrete_controller, continuous_controller], 0, 1)
+
+    # Assert
+    assert len(time_nodes) == 11
+    assert all(node._controllers == [discrete_controller] for node in time_nodes)
+    assert all(continuous_controller not in node._controllers for node in time_nodes)
+
+
 def test_time_nodes_sort(flight_calisto):
     time_nodes = flight_calisto.TimeNodes()
     time_nodes.add_node(3.0, [], [], [])
diff --git a/tests/unit/simulation/test_monte_carlo.py b/tests/unit/simulation/test_monte_carlo.py
index 5595e46bb..4e543505d 100644
--- a/tests/unit/simulation/test_monte_carlo.py
+++ b/tests/unit/simulation/test_monte_carlo.py
@@ -1,3 +1,8 @@
+import csv
+import json
+import pathlib
+from collections import namedtuple
+
 import matplotlib as plt
 import numpy as np
 import pytest
@@ -185,3 +190,326 @@ def test_estimate_confidence_interval_raises_type_error_for_invalid_statistic():
 
     with pytest.raises(TypeError):
         mc.estimate_confidence_interval("apogee", statistic="not_a_function")
+
+
+@pytest.mark.parametrize(
+    "kwargs, match",
+    [
+        ({"batch_size": 0}, "batch_size"),
+        ({"batch_size": -5}, "batch_size"),
+        ({"max_simulations": 0}, "max_simulations"),
+        ({"tolerance": 0}, "tolerance"),
+        ({"tolerance": -1.0}, "tolerance"),
+        ({"target_confidence": 1.5}, "target_confidence"),
+        ({"target_confidence": 0}, "target_confidence"),
+    ],
+)
+def test_simulate_convergence_validates_inputs(kwargs, match):
+    """simulate_convergence must reject invalid inputs up front. In particular a
+    non-positive batch_size would otherwise make the loop run zero simulations
+    per iteration and spin forever."""
+    mc = MockMonteCarlo()
+    with pytest.raises(ValueError, match=match):
+        mc.simulate_convergence(**kwargs)
+
+
+# --- CSV and JSON export/import tests ---
+
+
+class MockMonteCarloWithLogs(MonteCarlo):
+    """Mock class with populated logs for testing export/import methods."""
+
+    def __init__(self):
+        # pylint: disable=super-init-not-called
+        self.outputs_log = [
+            {"apogee": 5742.42, "x_impact": 553.49, "index": 0},
+            {"apogee": 3844.41, "x_impact": 402.31, "index": 1},
+            {"apogee": 4500.00, "x_impact": 480.10, "index": 2},
+        ]
+        self.inputs_log = [
+            {
+                "elevation": 1413.6,
+                "radius": 0.0635,
+                "parachutes": [{"cd_s": 9.84}],
+                "index": 0,
+            },
+            {
+                "elevation": 1400.0,
+                "radius": 0.0640,
+                "parachutes": [{"cd_s": 10.0}],
+                "index": 1,
+            },
+            {
+                "elevation": 1420.0,
+                "radius": 0.0630,
+                "parachutes": [{"cd_s": 9.50}],
+                "index": 2,
+            },
+        ]
+        self.errors_log = []
+        self.results = {}
+        self.processed_results = {}
+        self.num_of_loaded_sims = 3
+
+
+def test_export_outputs_to_csv(tmp_path):
+    """Tests that outputs are correctly exported to CSV."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.csv"
+
+    mc.export_outputs_to_csv(str(filepath))
+
+    with open(filepath, encoding="utf-8") as f:
+        reader = csv.DictReader(f)
+        rows = list(reader)
+
+    assert len(rows) == 3
+    assert float(rows[0]["apogee"]) == pytest.approx(5742.42)
+    assert float(rows[1]["x_impact"]) == pytest.approx(402.31)
+
+
+def test_export_outputs_to_json(tmp_path):
+    """Tests that outputs are correctly exported to JSON."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.json"
+
+    mc.export_outputs_to_json(str(filepath))
+
+    with open(filepath, encoding="utf-8") as f:
+        data = json.load(f)
+
+    assert len(data) == 3
+    assert data[0]["apogee"] == pytest.approx(5742.42)
+    assert data[2]["index"] == 2
+
+
+def test_export_inputs_to_csv_no_flatten(tmp_path):
+    """Tests that inputs with nested values are serialized as JSON in CSV cells."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "inputs.csv"
+
+    mc.export_inputs_to_csv(str(filepath), flatten=False)
+
+    with open(filepath, encoding="utf-8") as f:
+        reader = csv.DictReader(f)
+        rows = list(reader)
+
+    assert len(rows) == 3
+    # The parachutes column should contain a JSON string
+    parachutes_val = json.loads(rows[0]["parachutes"])
+    assert parachutes_val == [{"cd_s": 9.84}]
+
+
+def test_export_inputs_to_csv_flatten(tmp_path):
+    """Tests that flatten=True omits non-scalar columns."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "inputs.csv"
+
+    mc.export_inputs_to_csv(str(filepath), flatten=True)
+
+    with open(filepath, encoding="utf-8") as f:
+        reader = csv.DictReader(f)
+        rows = list(reader)
+
+    assert "parachutes" not in rows[0]
+    assert "elevation" in rows[0]
+    assert "radius" in rows[0]
+
+
+def test_export_inputs_to_json(tmp_path):
+    """Tests that inputs are correctly exported to JSON."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "inputs.json"
+
+    mc.export_inputs_to_json(str(filepath))
+
+    with open(filepath, encoding="utf-8") as f:
+        data = json.load(f)
+
+    assert len(data) == 3
+    assert data[0]["parachutes"] == [{"cd_s": 9.84}]
+
+
+def test_export_empty_log_raises_error(tmp_path):
+    """Tests that exporting an empty log raises ValueError."""
+    mc = MockMonteCarloWithLogs()
+    mc.outputs_log = []
+
+    with pytest.raises(ValueError, match="No data to export"):
+        mc.export_outputs_to_csv(str(tmp_path / "empty.csv"))
+
+    with pytest.raises(ValueError, match="No data to export"):
+        mc.export_outputs_to_json(str(tmp_path / "empty.json"))
+
+
+def test_import_outputs_from_csv(tmp_path):
+    """Tests that outputs can be imported from a CSV file."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.csv"
+
+    # Export first
+    mc.export_outputs_to_csv(str(filepath))
+
+    # Create a fresh mock and import
+    mc2 = MockMonteCarloWithLogs()
+    mc2.output_file = str(filepath)
+
+    assert len(mc2.outputs_log) == 3
+    assert mc2.outputs_log[0]["apogee"] == pytest.approx(5742.42)
+    assert mc2.outputs_log[1]["x_impact"] == pytest.approx(402.31)
+
+
+def test_import_outputs_from_json(tmp_path):
+    """Tests that outputs can be imported from a JSON file."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.json"
+
+    # Export first
+    mc.export_outputs_to_json(str(filepath))
+
+    # Create a fresh mock and import
+    mc2 = MockMonteCarloWithLogs()
+    mc2.output_file = str(filepath)
+
+    assert len(mc2.outputs_log) == 3
+    assert mc2.outputs_log[0]["apogee"] == pytest.approx(5742.42)
+
+
+def test_round_trip_outputs_csv(tmp_path):
+    """Tests that outputs survive a CSV export/import round trip."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.csv"
+
+    mc.export_outputs_to_csv(str(filepath))
+    mc.output_file = str(filepath)
+
+    for i, original in enumerate(MockMonteCarloWithLogs().outputs_log):
+        for key, value in original.items():
+            assert mc.outputs_log[i][key] == pytest.approx(value)
+
+
+def test_round_trip_outputs_json(tmp_path):
+    """Tests that outputs survive a JSON export/import round trip."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.json"
+
+    mc.export_outputs_to_json(str(filepath))
+    mc.output_file = str(filepath)
+
+    for i, original in enumerate(MockMonteCarloWithLogs().outputs_log):
+        for key, value in original.items():
+            assert mc.outputs_log[i][key] == pytest.approx(value)
+
+
+def test_round_trip_inputs_csv(tmp_path):
+    """Tests that inputs with nested values survive a CSV round trip."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "inputs.csv"
+
+    mc.export_inputs_to_csv(str(filepath), flatten=False)
+    mc.input_file = str(filepath)
+
+    assert mc.inputs_log[0]["parachutes"] == [{"cd_s": 9.84}]
+    assert mc.inputs_log[0]["elevation"] == pytest.approx(1413.6)
+
+
+def test_detect_file_format_unsupported():
+    """Tests that unsupported file extensions raise ValueError."""
+    mc = MockMonteCarloWithLogs()
+
+    with pytest.raises(ValueError, match="Unsupported file extension"):
+        mc._detect_file_format("data.xlsx")
+
+    with pytest.raises(ValueError, match="Unsupported file extension"):
+        mc._detect_file_format("data.parquet")
+
+
+def test_set_num_of_loaded_sims_csv(tmp_path):
+    """Tests that set_num_of_loaded_sims works with CSV files."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.csv"
+
+    mc.export_outputs_to_csv(str(filepath))
+    mc._output_file = str(filepath)
+    mc.set_num_of_loaded_sims()
+
+    assert mc.num_of_loaded_sims == 3
+
+
+def test_set_num_of_loaded_sims_json(tmp_path):
+    """Tests that set_num_of_loaded_sims works with JSON files."""
+    mc = MockMonteCarloWithLogs()
+    filepath = tmp_path / "outputs.json"
+
+    mc.export_outputs_to_json(str(filepath))
+    mc._output_file = str(filepath)
+    mc.set_num_of_loaded_sims()
+
+    assert mc.num_of_loaded_sims == 3
+
+
+# --- Adaptive Monte Carlo convergence (PR #922) ---
+
+_CI = namedtuple("_CI", ["low", "high"])
+
+
+class ConvergenceMockMonteCarlo(MonteCarlo):
+    """Mock that fakes batch simulation and a scripted confidence-interval
+    width, so ``simulate_convergence``'s stopping decision can be unit-tested
+    without running any real flight simulation."""
+
+    def __init__(self, width_model):
+        # pylint: disable=super-init-not-called
+        self.num_of_loaded_sims = 0
+        self.filename = pathlib.Path("dummy_mc")
+        self._width_model = width_model
+        self.simulate_calls = 0
+
+    def import_outputs(self, *args, **kwargs):  # no-op, avoids file I/O
+        pass
+
+    def simulate(self, number_of_simulations, append=True, **kwargs):
+        # pylint: disable=arguments-differ,unused-argument
+        self.simulate_calls += 1
+        self.num_of_loaded_sims = number_of_simulations
+
+    def estimate_confidence_interval(self, attribute, confidence_level=0.95, **kwargs):
+        # pylint: disable=arguments-differ,unused-argument
+        width = self._width_model(self.num_of_loaded_sims)
+        return _CI(low=0.0, high=width)
+
+
+def test_simulate_convergence_stops_early_when_tolerance_met():
+    """The convergence loop must stop as soon as the CI width drops below the
+    tolerance, well before reaching max_simulations."""
+    # width = 40 / n  ->  50 sims: 0.8 (> 0.5),  100 sims: 0.4 (<= 0.5) -> stop
+    mc = ConvergenceMockMonteCarlo(width_model=lambda n: 40.0 / n)
+
+    history = mc.simulate_convergence(
+        target_attribute="apogee_time",
+        tolerance=0.5,
+        max_simulations=1000,
+        batch_size=50,
+    )
+
+    assert history[-1] <= 0.5
+    assert len(history) == 2  # stopped after the second batch
+    assert mc.num_of_loaded_sims == 100
+    assert mc.num_of_loaded_sims < 1000  # did not exhaust the simulation budget
+
+
+def test_simulate_convergence_runs_until_max_when_not_converging():
+    """When the CI width never drops below the tolerance, the loop must run
+    until max_simulations and never exceed it."""
+    mc = ConvergenceMockMonteCarlo(width_model=lambda n: 10.0)  # constant, > tol
+
+    history = mc.simulate_convergence(
+        target_attribute="apogee_time",
+        tolerance=0.5,
+        max_simulations=200,
+        batch_size=50,
+    )
+
+    assert mc.num_of_loaded_sims == 200
+    assert all(width > 0.5 for width in history)
+    assert len(history) == 4  # 200 / 50 batches
diff --git a/tests/unit/stochastic/test_stochastic_model.py b/tests/unit/stochastic/test_stochastic_model.py
index 0d0a13311..9e35a5330 100644
--- a/tests/unit/stochastic/test_stochastic_model.py
+++ b/tests/unit/stochastic/test_stochastic_model.py
@@ -13,9 +13,11 @@
     ],
 )
 def test_visualize_attributes(request, fixture_name):
-    """Tests the visualize_attributes method of the StochasticModel class. This
-    test verifies if the method returns None, which means that the method is
-    running without breaking.
+    """Tests the visualize_attributes method of the StochasticModel class. It
+    must run without breaking and return the formatted report string (which is
+    also printed), so the report is never silently lost.
     """
     fixture = request.getfixturevalue(fixture_name)
-    assert fixture.visualize_attributes() is None
+    report = fixture.visualize_attributes()
+    assert isinstance(report, str)
+    assert report
diff --git a/tests/unit/stochastic/test_stochastic_parachute.py b/tests/unit/stochastic/test_stochastic_parachute.py
index 09a1497f7..01b5efb91 100644
--- a/tests/unit/stochastic/test_stochastic_parachute.py
+++ b/tests/unit/stochastic/test_stochastic_parachute.py
@@ -1,4 +1,4 @@
-from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.parachutes import HemisphericalParachute
 
 
 def test_stochastic_parachute_create_object(stochastic_main_parachute):
@@ -18,4 +18,4 @@ class creates a StochasticParachute object from the randomly generated
     None
     """
     obj = stochastic_main_parachute.create_object()
-    assert isinstance(obj, Parachute)
+    assert isinstance(obj, HemisphericalParachute)
diff --git a/tests/unit/test_encoders.py b/tests/unit/test_encoders.py
new file mode 100644
index 000000000..7f5c2f005
--- /dev/null
+++ b/tests/unit/test_encoders.py
@@ -0,0 +1,75 @@
+"""Unit tests for the RocketPy JSON encoder/decoder helpers."""
+
+import importlib
+import json
+import warnings
+
+import pytest
+
+from rocketpy._encoders import RocketPyDecoder, get_class_from_signature
+from rocketpy.rocket.parachutes import HemisphericalParachute, Parachute
+
+
+def test_get_class_from_signature_remaps_legacy_parachute():
+    """The legacy ``rocketpy.rocket.parachute.Parachute`` signature must remap to
+    the concrete ``HemisphericalParachute`` (the old module was moved and the
+    class became abstract)."""
+    legacy_signature = {
+        "module": "rocketpy.rocket.parachute",
+        "name": "Parachute",
+    }
+    assert get_class_from_signature(legacy_signature) is HemisphericalParachute
+
+
+def test_decode_legacy_parachute_rpy_reconstructs_object():
+    """Regression: parachutes saved in ``.rpy`` files by older versions used the
+    now-deleted ``rocketpy.rocket.parachute`` module path. They must still
+    reconstruct as a concrete parachute object instead of silently returning a
+    raw dict."""
+    legacy_entry = {
+        "signature": {"module": "rocketpy.rocket.parachute", "name": "Parachute"},
+        "name": "drogue",
+        "cd_s": 1.0,
+        "trigger": "apogee",
+        "sampling_rate": 105,
+        "lag": 1.5,
+        "noise": [0, 8.3, 0.5],
+        "radius": 0.5,
+        "drag_coefficient": 1.4,
+        "height": 0.5,
+        "porosity": 0.0432,
+    }
+
+    decoded = json.loads(json.dumps(legacy_entry), cls=RocketPyDecoder)
+
+    assert isinstance(decoded, Parachute)
+    assert isinstance(decoded, HemisphericalParachute)
+    assert decoded.name == "drogue"
+    assert decoded.cd_s == 1.0
+    assert decoded.lag == 1.5
+    assert callable(decoded.triggerfunc)
+
+
+def test_decoder_warns_on_unresolvable_signature():
+    """An unresolvable signature must surface a warning rather than silently
+    returning a raw dictionary (which previously masked data loss)."""
+    entry = {
+        "signature": {"module": "rocketpy.does_not_exist", "name": "Ghost"},
+        "value": 1,
+    }
+    with pytest.warns(UserWarning, match="Could not reconstruct"):
+        decoded = json.loads(json.dumps(entry), cls=RocketPyDecoder)
+    assert decoded == {"value": 1}
+
+
+def test_legacy_parachute_module_import_is_deprecated():
+    """Importing from the old ``rocketpy.rocket.parachute`` module path must
+    still work but emit a ``DeprecationWarning``."""
+    with warnings.catch_warnings():
+        warnings.simplefilter("error", DeprecationWarning)
+        with pytest.raises(DeprecationWarning):
+            importlib.reload(importlib.import_module("rocketpy.rocket.parachute"))
+
+    module = importlib.import_module("rocketpy.rocket.parachute")
+    assert module.Parachute is Parachute
+    assert module.HemisphericalParachute is HemisphericalParachute
diff --git a/tests/unit/test_flight_export_deprecation.py b/tests/unit/test_flight_export_deprecation.py
deleted file mode 100644
index 6fb6952b4..000000000
--- a/tests/unit/test_flight_export_deprecation.py
+++ /dev/null
@@ -1,40 +0,0 @@
-from unittest.mock import patch
-
-import pytest
-
-# TODO: these tests should be deleted after the deprecated methods are removed
-
-
-def test_export_data_deprecated_emits_warning_and_delegates(flight_calisto, tmp_path):
-    """Expect: calling Flight.export_data emits DeprecationWarning and delegates to FlightDataExporter.export_data."""
-    out = tmp_path / "out.csv"
-    with patch(
-        "rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_data"
-    ) as spy:
-        with pytest.warns(DeprecationWarning):
-            flight_calisto.export_data(str(out))
-    spy.assert_called_once()
-
-
-def test_export_pressures_deprecated_emits_warning_and_delegates(
-    flight_calisto_robust, tmp_path
-):
-    """Expect: calling Flight.export_pressures emits DeprecationWarning and delegates to FlightDataExporter.export_pressures."""
-    out = tmp_path / "p.csv"
-    with patch(
-        "rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_pressures"
-    ) as spy:
-        with pytest.warns(DeprecationWarning):
-            flight_calisto_robust.export_pressures(str(out), time_step=0.1)
-    spy.assert_called_once()
-
-
-def test_export_kml_deprecated_emits_warning_and_delegates(flight_calisto, tmp_path):
-    """Expect: calling Flight.export_kml emits DeprecationWarning and delegates to FlightDataExporter.export_kml."""
-    out = tmp_path / "traj.kml"
-    with patch(
-        "rocketpy.simulation.flight_data_exporter.FlightDataExporter.export_kml"
-    ) as spy:
-        with pytest.warns(DeprecationWarning):
-            flight_calisto.export_kml(str(out), time_step=0.5)
-    spy.assert_called_once()
diff --git a/tests/unit/test_parachute_triggers.py b/tests/unit/test_parachute_triggers.py
new file mode 100644
index 000000000..77ca55835
--- /dev/null
+++ b/tests/unit/test_parachute_triggers.py
@@ -0,0 +1,232 @@
+import numpy as np
+import pytest
+
+from rocketpy.rocket.parachutes import HemisphericalParachute
+from rocketpy.simulation.flight import Flight
+
+
+def test_trigger_receives_u_dot():
+    def derivative_func(_t, _y):
+        return np.array([0, 0, 0, 1.0, 2.0, 3.0, 0, 0, 0, 0, 0, 0, 0])
+
+    recorded = {}
+
+    def user_trigger(_p, _h, _y, u_dot):
+        recorded["u_dot"] = np.array(u_dot)
+        return True
+
+    parachute = HemisphericalParachute(
+        name="test",
+        cd_s=1.0,
+        trigger=user_trigger,
+        sampling_rate=100,
+    )
+
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=10.0,
+        y=np.zeros(13),
+        sensors=[],
+        derivative_func=derivative_func,
+        t=0.0,
+    )
+
+    assert res is True
+    assert "u_dot" in recorded
+    assert np.allclose(recorded["u_dot"][3:6], np.array([1.0, 2.0, 3.0]))
+
+
+def test_trigger_with_u_dot_only():
+    """Test trigger that only expects u_dot (no sensors)."""
+
+    def derivative_func(_t, _y):
+        return np.array([0, 0, 0, -1.0, -2.0, -3.0, 0, 0, 0, 0, 0, 0, 0])
+
+    recorded = {}
+
+    def user_trigger(_p, _h, _y, u_dot):
+        recorded["u_dot"] = np.array(u_dot)
+        return False
+
+    parachute = HemisphericalParachute(
+        name="test_u_dot_only",
+        cd_s=1.0,
+        trigger=user_trigger,
+        sampling_rate=100,
+    )
+
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=5.0,
+        y=np.zeros(13),
+        sensors=[],
+        derivative_func=derivative_func,
+        t=1.234,
+    )
+
+    assert res is False
+    assert "u_dot" in recorded
+    assert np.allclose(recorded["u_dot"][3:6], np.array([-1.0, -2.0, -3.0]))
+
+
+def test_basic_trigger_does_not_compute_u_dot():
+    def derivative_func(_t, _y):
+        raise RuntimeError("derivative should not be called for legacy triggers")
+
+    called = {}
+
+    def basic_trigger(_p, _h, _y):
+        called["ok"] = True
+        return True
+
+    parachute = HemisphericalParachute(
+        name="basic",
+        cd_s=1.0,
+        trigger=basic_trigger,
+        sampling_rate=100,
+    )
+
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=0.0,
+        y=np.zeros(13),
+        sensors=[],
+        derivative_func=derivative_func,
+        t=0.0,
+    )
+
+    assert res is True
+    assert called.get("ok", False) is True
+
+
+def test_five_arg_trigger_with_descriptive_names_receives_u_dot():
+    """Regression: a documented 5-arg trigger (p, h, y, sensors, u_dot) with
+    descriptive parameter names must still receive a valid (non-None) u_dot.
+    u_dot delivery used to be gated on the parameter NAME, so such triggers
+    silently received u_dot=None and crashed."""
+
+    def derivative_func(_t, _y):
+        return np.array([0, 0, 0, 4.0, 5.0, 6.0, 0, 0, 0, 0, 0, 0, 0])
+
+    recorded = {}
+
+    def user_trigger(  # pylint: disable=unused-argument
+        pressure, altitude, state, sensor_list, state_derivative
+    ):
+        recorded["u_dot"] = (
+            None if state_derivative is None else np.array(state_derivative)
+        )
+        return True
+
+    parachute = HemisphericalParachute(
+        name="five_arg", cd_s=1.0, trigger=user_trigger, sampling_rate=100
+    )
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=10.0,
+        y=np.zeros(13),
+        sensors=[],
+        derivative_func=derivative_func,
+        t=0.0,
+    )
+
+    assert res is True
+    assert recorded["u_dot"] is not None
+    assert np.allclose(recorded["u_dot"][3:6], np.array([4.0, 5.0, 6.0]))
+
+
+def test_four_arg_acceleration_trigger_by_name_receives_u_dot():
+    """A 4-arg trigger whose 4th parameter is named like an acceleration must
+    receive u_dot (name-based disambiguation is retained only for the ambiguous
+    4-arg case)."""
+
+    def derivative_func(_t, _y):
+        return np.array([0, 0, 0, -9.0, 0, 0, 0, 0, 0, 0, 0, 0, 0])
+
+    recorded = {}
+
+    def user_trigger(_p, _h, _y, acceleration):
+        recorded["val"] = None if acceleration is None else np.array(acceleration)
+        return True
+
+    parachute = HemisphericalParachute(
+        name="four_arg_acc", cd_s=1.0, trigger=user_trigger, sampling_rate=100
+    )
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=1.0,
+        y=np.zeros(13),
+        sensors=["S"],
+        derivative_func=derivative_func,
+        t=0.0,
+    )
+
+    assert res is True
+    assert recorded["val"] is not None
+    assert recorded["val"][3] == -9.0
+
+
+def test_four_arg_sensors_trigger_receives_sensors():
+    """A 4-arg trigger whose 4th parameter is named 'sensors' must receive the
+    sensors list and must NOT trigger u_dot computation."""
+
+    def derivative_func(_t, _y):
+        raise RuntimeError("u_dot should not be computed for a sensors trigger")
+
+    recorded = {}
+
+    def user_trigger(_p, _h, _y, sensors):
+        recorded["sensors"] = sensors
+        return False
+
+    parachute = HemisphericalParachute(
+        name="four_arg_sensors", cd_s=1.0, trigger=user_trigger, sampling_rate=100
+    )
+    dummy = type("D", (), {})()
+
+    res = Flight._evaluate_parachute_trigger(
+        dummy,
+        parachute,
+        pressure=0.0,
+        height=1.0,
+        y=np.zeros(13),
+        sensors=["A", "B"],
+        derivative_func=derivative_func,
+        t=0.0,
+    )
+
+    assert res is False
+    assert recorded["sensors"] == ["A", "B"]
+
+
+def test_invalid_arity_trigger_raises_at_construction():
+    """A trigger with fewer than 3 parameters must fail fast at construction
+    rather than mid-simulation."""
+
+    def bad_trigger(_p, _h):
+        return True
+
+    with pytest.raises(TypeError, match="unsupported signature"):
+        HemisphericalParachute(
+            name="bad", cd_s=1.0, trigger=bad_trigger, sampling_rate=100
+        )
diff --git a/tests/unit/test_plots.py b/tests/unit/test_plots.py
index fc412d3b9..d173a0837 100644
--- a/tests/unit/test_plots.py
+++ b/tests/unit/test_plots.py
@@ -1,4 +1,7 @@
+import builtins
 import os
+import sys
+import types
 from unittest.mock import MagicMock, patch
 
 import matplotlib.pyplot as plt
@@ -171,3 +174,200 @@ def test_animate_fluid_volume(example_mass_flow_rate_based_tank_seblm):
     assert os.path.exists("test_fluid_volume.gif")
 
     os.remove("test_fluid_volume.gif")
+
+
+class _DummyVedoActor:
+    """Minimal actor mock that supports the methods used by animation plots."""
+
+    def __init__(self):
+        self.rotations = []
+
+    def c(self, *_args, **_kwargs):
+        return self
+
+    def pos(self, *_args, **_kwargs):
+        return self
+
+    def wireframe(self):
+        return self
+
+    def rotate(self, angle, axis=None, point=None):
+        self.rotations.append((angle, axis, point))
+        return self
+
+    def clone(self):
+        return _DummyVedoActor()
+
+
+class _DummyPlotter:
+    """Minimal plotter mock for non-interactive animation tests."""
+
+    def __init__(self, *_args, **_kwargs):
+        self.escaped = False
+
+    def show(self, *_args, **_kwargs):
+        return self
+
+    def render(self):
+        return None
+
+    def interactive(self):
+        return self
+
+    def close(self):
+        return None
+
+
+def _mock_vedo_module(monkeypatch):
+    """Install a minimal vedo module in sys.modules for tests."""
+
+    vedo_module = types.ModuleType("vedo")
+    vedo_module.Mesh = lambda *_args, **_kwargs: _DummyVedoActor()
+    vedo_module.Box = lambda *_args, **_kwargs: _DummyVedoActor()
+    vedo_module.Line = lambda *_args, **_kwargs: _DummyVedoActor()
+    vedo_module.Plotter = _DummyPlotter
+    vedo_module.settings = types.SimpleNamespace()
+    monkeypatch.setitem(sys.modules, "vedo", vedo_module)
+
+
+def test_animate_trajectory_runs_with_mocked_vedo(flight_calisto, monkeypatch):
+    """Test flight trajectory animation entry point through the plots layer."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+
+    # Act
+    result = flight_calisto.plots.animate_trajectory(
+        start=0.0,
+        stop=0.001,
+        time_step=0.001,
+    )
+
+    # Assert
+    assert result is None
+
+
+def test_animate_rotate_runs_with_mocked_vedo(flight_calisto, monkeypatch):
+    """Test flight rotation animation entry point through the plots layer."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+
+    # Act
+    result = flight_calisto.plots.animate_rotate(
+        start=0.0,
+        stop=0.001,
+        time_step=0.001,
+    )
+
+    # Assert
+    assert result is None
+
+
+def test_animate_trajectory_raises_when_vedo_is_missing(flight_calisto, monkeypatch):
+    """Test that an informative ImportError is raised when vedo is unavailable."""
+
+    # Arrange
+    real_import = builtins.__import__
+
+    def import_without_vedo(name, *args, **kwargs):
+        if name == "vedo" or name.startswith("vedo."):
+            raise ImportError("No module named 'vedo'")
+        return real_import(name, *args, **kwargs)
+
+    monkeypatch.setattr(builtins, "__import__", import_without_vedo)
+
+    # Act / Assert
+    with pytest.raises(ImportError, match="optional dependency"):
+        flight_calisto.plots.animate_trajectory(
+            start=0.0,
+            stop=0.001,
+            time_step=0.001,
+        )
+
+
+def test_animate_rotate_raises_when_time_range_is_invalid(flight_calisto, monkeypatch):
+    """Test validation error for invalid animation time range."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+    # Act / Assert
+    with pytest.raises(ValueError, match="Invalid animation time range"):
+        flight_calisto.plots.animate_rotate(
+            start=1.0,
+            stop=0.5,
+            time_step=0.1,
+        )
+
+
+def test_animate_trajectory_raises_when_stl_file_is_missing(
+    flight_calisto, monkeypatch
+):
+    """Test file validation when STL path does not exist."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+
+    # Act / Assert
+    with pytest.raises(FileNotFoundError, match="Could not find the 3D model file"):
+        flight_calisto.plots.animate_trajectory(
+            "missing_model.stl",
+            start=0.0,
+            stop=0.1,
+            time_step=0.1,
+        )
+
+
+@pytest.mark.parametrize("invalid_time_step", [0, -0.1])
+def test_animate_trajectory_raises_when_time_step_is_non_positive(
+    flight_calisto, monkeypatch, invalid_time_step
+):
+    """Test validation error when animation time_step is not strictly positive."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+    # Act / Assert
+    with pytest.raises(ValueError, match="Invalid time_step"):
+        flight_calisto.plots.animate_trajectory(
+            start=0.0,
+            stop=0.1,
+            time_step=invalid_time_step,
+        )
+
+
+def test_animate_rotate_raises_when_stop_exceeds_flight_end(
+    flight_calisto, monkeypatch
+):
+    """Test validation error when stop time exceeds available simulation range."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+    # Act / Assert
+    with pytest.raises(ValueError, match="Invalid animation time range"):
+        flight_calisto.plots.animate_rotate(
+            start=0.0,
+            stop=flight_calisto.t_final + 0.1,
+            time_step=0.1,
+        )
+
+
+def test_animate_trajectory_raises_when_default_model_is_missing(
+    flight_calisto, monkeypatch
+):
+    """Test failure path when default packaged STL model is unavailable."""
+
+    # Arrange
+    _mock_vedo_module(monkeypatch)
+    monkeypatch.setattr(
+        flight_calisto.plots,
+        "_resolve_animation_model_path",
+        lambda _file_name: "missing_default_model.stl",
+    )
+
+    # Act / Assert
+    with pytest.raises(FileNotFoundError, match="Could not find the 3D model file"):
+        flight_calisto.plots.animate_trajectory(
+            start=0.0,
+            stop=0.1,
+            time_step=0.1,
+        )
diff --git a/tests/unit/test_rail_buttons_bending_moments.py b/tests/unit/test_rail_buttons_bending_moments.py
index b61720d3d..50336fdbc 100644
--- a/tests/unit/test_rail_buttons_bending_moments.py
+++ b/tests/unit/test_rail_buttons_bending_moments.py
@@ -4,6 +4,7 @@
 of the calculate_rail_button_bending_moments method in isolation.
 """
 
+import logging
 import warnings
 
 import matplotlib.pyplot as plt
@@ -199,24 +200,20 @@ def test_rail_button_bending_moments_plot_with_height(flight_calisto_robust):
     plt.close("all")
 
 
-def test_rail_button_bending_moments_plot_without_height(flight_calisto_robust, capsys):
+def test_rail_button_bending_moments_plot_without_height(flight_calisto_robust, caplog):
     """Test that bending moments plot is skipped when button_height is None.
 
     Parameters
     ----------
     flight_calisto_robust : rocketpy.Flight
         Flight fixture with motor and rail buttons.
-    capsys : pytest fixture
-        Captures stdout/stderr.
+    caplog : pytest fixture
+        Captures log records.
     """
     # Ensure button_height is None (it should be by default now)
     flight_calisto_robust.rocket.rail_buttons[0].component.button_height = None
 
-    # Call plot method
-    flight_calisto_robust.plots.rail_buttons_bending_moments()
-
-    # Capture output
-    captured = capsys.readouterr()
+    with caplog.at_level(logging.WARNING, logger="rocketpy"):
+        flight_calisto_robust.plots.rail_buttons_bending_moments()
 
-    # Should print skip message
-    assert "height not defined" in captured.out
+    assert "height not defined" in caplog.text
diff --git a/tests/unit/test_tools.py b/tests/unit/test_tools.py
index fcf67ad37..a1e96eb9e 100644
--- a/tests/unit/test_tools.py
+++ b/tests/unit/test_tools.py
@@ -1,6 +1,7 @@
 import numpy as np
 import pytest
 
+from rocketpy import Environment
 from rocketpy.tools import (
     calculate_cubic_hermite_coefficients,
     euler313_to_quaternions,
@@ -100,3 +101,39 @@ def test_tuple_handler(input_value, expected_output):
 def test_tuple_handler_exceptions(input_value, expected_exception):
     with pytest.raises(expected_exception):
         tuple_handler(input_value)
+
+
+@pytest.mark.parametrize("pressure_conversion_factor", ["hPa", "mbar", "Pa", 100])
+def test_valid_pressure_conversion_factor(pressure_conversion_factor):
+    env = Environment(
+        gravity=9.81,
+        latitude=47.213476,
+        longitude=9.003336,
+        date=(2020, 2, 22, 13),
+        elevation=407,
+    )
+    env.set_atmospheric_model(
+        type="Reanalysis",
+        file="data/weather/bella_lui_weather_data_ERA5.nc",
+        dictionary="ECMWF",
+        pressure_conversion_factor=pressure_conversion_factor,
+    )
+
+
+@pytest.mark.parametrize("pressure_conversion_factor", [-1, "mPa"])
+def test_invalid_pressure_conversion_factor(pressure_conversion_factor):
+    env = Environment(
+        gravity=9.81,
+        latitude=47.213476,
+        longitude=9.003336,
+        date=(2020, 2, 22, 13),
+        elevation=407,
+    )
+
+    with pytest.raises(ValueError):
+        env.set_atmospheric_model(
+            type="Reanalysis",
+            file="data/weather/bella_lui_weather_data_ERA5.nc",
+            dictionary="ECMWF",
+            pressure_conversion_factor=pressure_conversion_factor,
+        )
diff --git a/tests/unit/test_utilities.py b/tests/unit/test_utilities.py
index ce85f01de..6b2eb7d5a 100644
--- a/tests/unit/test_utilities.py
+++ b/tests/unit/test_utilities.py
@@ -1,3 +1,4 @@
+import logging
 import os
 from unittest.mock import patch
 
@@ -117,6 +118,19 @@ def test_fin_flutter_analysis(flight_calisto_custom_wind):
     assert np.isclose(safety_factor(np.inf), 61.669562809629035, atol=5e-3)
 
 
+def test_calculate_stall_wind_velocity_returns_value(flight_calisto_custom_wind):
+    """Regression: the stall wind velocity must be returned (it was previously
+    only logged at INFO level and the method returned None, losing the value).
+    The Flight method and the utilities function must agree."""
+    with pytest.warns(DeprecationWarning):
+        w_v = flight_calisto_custom_wind.calculate_stall_wind_velocity(5)
+    assert isinstance(w_v, float)
+    assert w_v > 0
+    assert utilities.calculate_stall_wind_velocity(
+        flight_calisto_custom_wind, 5
+    ) == pytest.approx(w_v)
+
+
 def test_fin_flutter_analysis_with_prints(flight_calisto_custom_wind):
     """Test fin_flutter_analysis with see_prints=True to cover print branch.
 
@@ -150,16 +164,17 @@ def test_fin_flutter_analysis_with_graphs(mock_show, flight_calisto_custom_wind)
     flight_calisto_custom_wind : Flight
         A Flight object with a rocket with fins.
     """
-    result = utilities.fin_flutter_analysis(
+    flutter_mach, safety_factor = utilities.fin_flutter_analysis(
         fin_thickness=2 / 1000,
         shear_modulus=10e9,
         flight=flight_calisto_custom_wind,
         see_prints=False,
-        see_graphs=True,  # True = returns None!
+        see_graphs=True,
         filename=None,
     )
 
-    assert result is None
+    assert isinstance(flutter_mach, Function)
+    assert isinstance(safety_factor, Function)
     mock_show.assert_called()
 
 
@@ -174,16 +189,19 @@ def test_fin_flutter_analysis_complete_output(mock_show, flight_calisto_custom_w
     flight_calisto_custom_wind : Flight
         A Flight object with a rocket with fins.
     """
-    result = utilities.fin_flutter_analysis(
+    flutter_mach, safety_factor = utilities.fin_flutter_analysis(
         fin_thickness=2 / 1000,
         shear_modulus=10e9,
         flight=flight_calisto_custom_wind,
         see_prints=True,
-        see_graphs=True,  # True = returns None!
+        see_graphs=True,
         filename=None,
     )
 
-    assert result is None
+    # The flutter Mach number and safety factor are always returned, regardless
+    # of see_prints/see_graphs, so the safety-critical results are never lost.
+    assert isinstance(flutter_mach, Function)
+    assert isinstance(safety_factor, Function)
     mock_show.assert_called()
 
 
@@ -328,3 +346,79 @@ def test_load_from_rpy(mock_show):  # pylint: disable=unused-argument
     )
     assert loaded_flight.info() is None
     assert loaded_flight.all_info() is None
+
+
+# --- Logging (rocketpy.utilities.enable_logging) ------------------------------
+
+
+@pytest.fixture(autouse=True)
+def reset_rocketpy_logger():
+    """Reset the rocketpy logger to its original state after each test."""
+    logger = logging.getLogger("rocketpy")
+    original_level = logger.level
+    original_handlers = logger.handlers[:]
+    yield
+    logger.handlers = original_handlers
+    logger.setLevel(original_level)
+
+
+def test_enable_logging_adds_stream_handler():
+    """enable_logging() must attach a StreamHandler to the rocketpy logger."""
+    utilities.enable_logging(level="INFO")
+
+    logger = logging.getLogger("rocketpy")
+    stream_handlers = [
+        h for h in logger.handlers if isinstance(h, logging.StreamHandler)
+    ]
+    assert len(stream_handlers) >= 1
+
+
+def test_enable_logging_sets_correct_level():
+    """enable_logging() must set the requested level on the rocketpy logger."""
+    utilities.enable_logging(level="DEBUG")
+    assert logging.getLogger("rocketpy").level == logging.DEBUG
+
+    utilities.enable_logging(level="WARNING")
+    assert logging.getLogger("rocketpy").level == logging.WARNING
+
+
+def test_enable_logging_no_duplicate_handlers():
+    """Calling enable_logging() twice must not duplicate StreamHandlers."""
+    utilities.enable_logging(level="INFO")
+    utilities.enable_logging(level="INFO")
+
+    logger = logging.getLogger("rocketpy")
+    stream_handlers = [
+        h for h in logger.handlers if isinstance(h, logging.StreamHandler)
+    ]
+    assert len(stream_handlers) == 1
+
+
+def test_enable_logging_replaces_handler_on_level_change():
+    """Calling enable_logging() with a new level must replace the old handler."""
+    utilities.enable_logging(level="WARNING")
+    utilities.enable_logging(level="DEBUG")
+
+    logger = logging.getLogger("rocketpy")
+    stream_handlers = [
+        h for h in logger.handlers if isinstance(h, logging.StreamHandler)
+    ]
+    assert len(stream_handlers) == 1
+    assert logger.level == logging.DEBUG
+
+
+def test_enable_logging_invalid_level_raises():
+    """enable_logging() must raise ValueError for an unrecognised level string."""
+    with pytest.raises(ValueError, match="Invalid logging level"):
+        utilities.enable_logging(level="INVALID")
+
+
+def test_enable_logging_messages_are_captured(caplog):
+    """After enable_logging(), internal rocketpy log messages must be visible."""
+    utilities.enable_logging(level="DEBUG")
+
+    with caplog.at_level(logging.DEBUG, logger="rocketpy"):
+        logger = logging.getLogger("rocketpy.simulation.flight")
+        logger.info("test message from flight")
+
+    assert "test message from flight" in caplog.text