Rocketprops Models Liquid Rocket Propellants

See the Code at:

See the Docs at:

See PyPI page at:

RocketProps calculates the various liquid propellant properties required to analyze 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.



Indices and tables