RocketPy

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**Is your feature request related to a problem? Please describe.** Right now, RocketPy has compatibility with ERA-5 reanalysis files from ESA only. **Describe the solution you'd like** It would be...

LUCKIN13

ENH: Enable only radial burning

3

## Pull request type - [X] Code changes (bugfix, features) ## Checklist - [ ] Lint (`black rocketpy/ tests/`) has passed locally - [ ] All tests (`pytest tests -m...

caioessouza

Currently we use the rocket's total center of pressure to compute the stability margin of the Flight class. Since this center of pressure is defined based on the normal force...

MateusStano

ENH: Individual Fins

1

## Checklist - [ ] Tests for the changes have been added (if needed) ## Description Individual Fins model have been added: - Usage can be seen in the documentation...

MateusStano

ENH: create a dataset of pre-registered motors.

6

## Pull request type - [x] Code changes (bugfix, features) - [x] Code maintenance (refactoring, formatting, tests) - [x] ReadMe, Docs and GitHub updates - [ ] Other (please describe):...

leogrosa

ENH: Tube Fins

1

I'm attempting to simulate the design for my Level 3 to try and find the maximum velocity, however rocketpy lacks any settings for tube fins. Can there be tube fins...

AlexKari

ENH: Enable only radial burning

4

**Is your feature request related to a problem? Please describe.** Rocketpy SolidMotor class only simulates radial and axial simoultaneos burn, but the regression rate on hybrid motor are modeled to...

caioessouza

ENH: Add the Coriolis Acceleration

5

I noticed that RocketPy currently doesn’t account for Coriolis effects in its equations. I made a few local modifications to include this behavior and found that, for a rocket with...

kevin-alcaniz

BUG: Paralle Monte Carlo simulation giving incorrect iterations

3

When running the parallel Monte Carlo simulations, there is a printout that shows the current iterations, iteration runtime, and estimated time left. When running in parallel, though, the value goes...

emtee14

**Describe the bug** When simulating a `Rocket` with two `Parachute` instances in the `Flight` class and setting the `time_overshoot` attribute to `False`, several functions return undefined values: `stability_margin`, `mach_number`, `free_stream_speed`,...

kevin-alcaniz