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RocketProps models liquid rocket propellants.

Project description

Rocketprops Models Liquid Rocket Propellants

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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.

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