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.