火箭推进器是液体火箭推进剂的模型。
rocketprops的Python项目详细描述
Rocketprops Models Liquid Rocket Propellants
See the Code at: https://github.com/sonofeft/RocketProps
See the Docs at: http://rocketprops.readthedocs.org/en/latest/
See PyPI page at:https://pypi.python.org/pypi/rocketprops
RocketProps calculates the various liquid propellant properties required
to analyse a liquid propellant thrust chamber.
This includes density, viscosity, vapor pressure,
heat of vaporization, surface tension, heat capacity and thermal conductivity.
Other properties such as critical temperature and pressure, normal boiling point,
molecular weight and freezing temperature are available.
关键词:rocketprops设置工具开发 站台:任何 分类器:开发状态::4-Beta 分类器:操作系统::独立于操作系统 分类器:目标受众::开发者 分类器:目标受众::最终用户/桌面 分类器:主题::软件开发::构建工具 分类器:License::OSI Approved::GNU General Public License v3(GPLv3) 分类器:编程语言::Python::3 分类器:编程语言::Python::3.5 分类器:编程语言::Python::3.6 分类器:编程语言::Python::3.7 分类器:编程语言::Python::3.8 类型:文本描述 提供额外的:dev 提供额外:测试
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