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Source: rocketcea
Section: science
Priority: optional
Maintainer: Bdale Garbee <bdale@gag.com>
Rules-Requires-Root: no
Build-Depends:
debhelper-compat (= 13),
dh-sequence-python3,
gfortran,
pkgconf,
pybuild-plugin-pyproject,
python3-dev,
python3-matplotlib,
python3-mesonpy,
python3-numpy,
python3-scipy,
python3-setuptools,
python3-sphinx
#Testsuite: autopkgtest-pkg-python
Standards-Version: 4.7.0
Homepage: https://rocketcea.readthedocs.io
Vcs-Browser: https://salsa.debian.org/debian/rocketcea
Vcs-Git: https://salsa.debian.org/debian/rocketcea.git
Package: rocketcea
Architecture: any
Depends:
${misc:Depends},
${python3:Depends},
${shlibs:Depends},
${sphinxdoc:Depends}
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.
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