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