Python package that helps engineers design rockets and rocket engines precisely and efficiently
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Updated
Dec 14, 2025 - Python
Python package that helps engineers design rockets and rocket engines precisely and efficiently
A Python library for the Steem Blockchain
Set of Python classes that allows computations for contours of supersonic nozzles
modern rocket design software for amateur rocketry
Solution of compressible flow inside a CD nozzle with shock formation. Implementation with Mac-Cormack scheme
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
SymPy-based lab for 1D vertical rocket mechanics: symbolic equations of motion, Tsiolkovsky Δv, and simple numeric experiments.
SymPy-based lab for quasi-1D nozzle gasdynamics: symbolic isentropic relations, numerical profiles, and engineering plots.
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+.
🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.
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