rocketcea

NASA Chemical Equilibrium, wrapped in Python

Description

RocketCEA makes direct calls to a modified copy of the NASA FORTRAN CEA code in “rocket” mode to calculate Isp, Cstar, Tcham etc. and provides tools to help determine useful mixture ratio range, optimum MR and more.

The modifications to CEA2.f have been made in order to properly handle hydrazine monopropellant’s ammonia dissociation.

A typical use of this program would be to help determine input values for a rocket motor burn simulation program.

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Homepage

https://rocketcea.readthedocs.io


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