rocketcea - 1.1.18+dfsg-3+b1 main

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.
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The modifications to CEA2.f have been made in order to properly handle
hydrazine monopropellant’s ammonia dissociation.
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A typical use of this program would be to help determine input values for a
rocket motor burn simulation program.