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thrust-to-weight

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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

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