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rocket-propulsion

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SvetLuna-Lab / -Liquid-Propellant-Rocket-Engine-Concept-for-Orbital-Launch-Vehicles-

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Conceptual design and analysis of a liquid-propellant rocket engine for orbital launch vehicles. Presents key specs (chamber pressure, nozzle expansion, thrust-to-weight), propellant/material selection (LOX/RP-1 & LOX/LH₂), cycle considerations, and computational workflows for engine sizing, sweeps and trade-off studies.

aerospace cea rocket-engine nozzle-design engine-design rocket-propulsion liquid-propellant orbital-launch-vehicle combustion-chamber thrust-to-weight lox-rp1 lox-lh2 propulsion-analysis spacecraft-engineering
  • Updated Nov 6, 2025
  • Python

Sarvesh2304 / Combustion_Simulation

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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
  • Updated Aug 26, 2025
  • Python

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