deb_control_files:
- control
- md5sums
- postinst
- prerm
deb_fields:
Architecture: amd64
Depends: python3-numpy (>= 1:1.25.0), python3-numpy-abi9, python3 (<< 3.13), python3
(>= 3.12~), python3-matplotlib, python3-scipy, python3:any, libc6 (>= 2.29), libgfortran5
(>= 8), libjs-sphinxdoc (>= 8.1)
Description: "NASA Chemical Equilibrium, wrapped in Python\n RocketCEA can be used\
\ to help determine input values for a rocket motor burn\n simulation program,\
\ like openmotor. The calculation engine is a modified\n copy of NASA's \"Chemical\
\ Equilibrium with Applications\" (CEA) FORTRAN code.\n .\n RocketCEA makes direct\
\ calls to a modified copy of the NASA FORTRAN CEA\n code in \u201Crocket\u201D\
\ mode to calculate Isp, Cstar, Tcham etc. and provides\n tools to help determine\
\ useful mixture ratio range, optimum MR and more.\n .\n The modifications to\
\ CEA2.f allow the program to properly handle hydrazine\n monopropellant\u2019\
s ammonia dissociation."
Homepage: https://rocketcea.readthedocs.io
Installed-Size: '30325'
Maintainer: Bdale Garbee <bdale@gag.com>
Package: rocketcea
Priority: optional
Section: science
Version: 1.2.1-2
srcpkg_name: rocketcea
srcpkg_version: 1.2.1-2