[ 原始碼： rocketcea ]
套件：rocketcea（1.2.1-2）
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.
其他與 rocketcea 有關的套件
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- dep: libc6 (>= 2.29)
- GNU C 函式庫：共用函式庫
同時作為一個虛擬套件由這些套件填實： libc6-udeb
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- dep: libgfortran5 (>= 8)
- Runtime library for GNU Fortran applications
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- dep: libjs-sphinxdoc (>= 8.1)
- JavaScript support for Sphinx documentation
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- dep: python3
- interactive high-level object-oriented language (default python3 version)
- dep: python3 (<< 3.13)
- dep: python3 (>= 3.12~)
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- dep: python3-matplotlib
- Python based plotting system in a style similar to Matlab
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- dep: python3-numpy (>= 1:1.25.0)
- Fast array facility to the Python language (Python 3)
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- dep: python3-numpy-abi9
- 本虛擬套件由這些套件填實： python3-numpy
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- dep: python3-scipy
- scientific tools for Python 3