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.