Package: rocketcea
Version: 1.2.1-2build2
Architecture: amd64
Maintainer: Ubuntu Developers <ubuntu-devel-discuss@lists.ubuntu.com>
Original-Maintainer: Bdale Garbee <bdale@gag.com>
Installed-Size: 30377
Depends: python3-numpy2-abi0 | python3-numpy-abi9, python3 (<< 3.14), python3 (>= 3.13~), python3-matplotlib, python3-numpy, python3-scipy, python3:any, libc6 (>= 2.29), libgfortran5 (>= 8), libjs-sphinxdoc (>= 8.1)
Section: science
Priority: optional
Homepage: https://rocketcea.readthedocs.io
Description: NASA Chemical Equilibrium, wrapped in Python
 RocketCEA can be used to help determine input values for a rocket motor burn
 simulation program, like openmotor.  The calculation engine is a modified
 copy of NASA's "Chemical Equilibrium with Applications" (CEA) FORTRAN code.
 .
 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 allow the program to properly handle hydrazine
 monopropellant’s ammonia dissociation.
