Python library for internal contour development and performance calculations of liquid propellant rocket engines - Under Development
https://github.com/juliomachad0/LPREpy
- Initial_Parameters
- Input_Propellant_CEAconfig
- Input_CEA_parameters
- Chamber_Profile
- Nozzle_Profile
- Inner_Profile
- Injectors design (impingement jet, swirl, pintle)
- Characteristic Length Calculation
- Regeneration (jaquet) Cooling calculation