Rocket Team Standard Atmosphere Model
Python module for computing atmospheric properties (T, P, ρ, speed of sound, from 0–110 km, anchored to actual launch-day ground
conditions instead of standard sea-level values as provided in US76
Reference information: 19770009539.pdf
**Repo:** https://github.com/shri-th/rocket-team-atmosphere-model.git
**Quick start:**
```bash
git clone https://github.com/shri-th/rocket-team-atmosphere-model.git
cd [repo-name]
pip install -r requirements.txt (check README and requirements.txt for full dependencies)
python plots.py
```
Edit `launch_site.py` (or the top of `plots.py`) with your measured pad
altitude, temperature, and pressure before running.
Want to contribute changes? Fork the repo and open a pull request, or ping
[your name] for collaborator access.
