25/06/2026
Excited to share my first open source Python package: AeroProp-X.
AeroProp-X is a physics based rocket nozzle design toolkit built using the Method of Characteristics. It helps engineers and researchers generate optimized nozzle contours, analyze flow fields, estimate performance, and export CAD ready designs for early stage aerospace development.
You can explore the package on PyPI.
https://pypi.org/project/aeroprop-x/
Install with:
pip install aeroprop-x
This is just the beginning, and I look forward to improving it with community feedback. If you're interested in aerospace engineering, computational physics, or scientific computing, I'd love to hear your thoughts.