specific-impulse

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SvetLuna-Lab / Nozzle-perf-estimator-demo

Minimal estimator of ideal (isentropic) rocket nozzle performance: exit state (Me, Pe, Te), CF, Isp, F/At, with Pc–area-ratio sweeps. Pure Python, small tests, CSV output for quick trade studies. Requires Python 3.10+.

python engineering gas-dynamics thrust nozzle rocketry demo-project compressible-flow isentropic aerothermodynamics rocket-propulsion specific-impulse

Updated Nov 13, 2025
Python

ellisdee14 / Nozzle-perf-estimator-demo

Star

🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.

python engineering gas-dynamics thrust nozzle rocketry demo-project compressible-flow isentropic aerothermodynamics rocket-propulsion specific-impulse

Updated Sep 8, 2026
Python

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