Physics-informed propellant combustion and nozzle performance simulator with an optional TensorFlow surrogate for specific impulse. Computes exhaust velocity, thrust, Isp, temp/pressure profiles, wall heating, and stability spectrum for multiple propellants. CLI, plots, and cached models in models
python machine-learning neural-network tensorflow numpy thermodynamics scipy matplotlib cfd combustion-models finite-rate-chemistry aerospace-applications propellant-data aerospace-simulator comustion-simulation rocket-propulsion propellant-analysis aeropace-engineering
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Updated
Aug 26, 2025 - Python