# RocketProps

**Repository Path**: openminds/RocketProps

## Basic Information

- **Project Name**: RocketProps
- **Description**: No description available
- **Primary Language**: Unknown
- **License**: GPL-3.0
- **Default Branch**: master
- **Homepage**: None
- **GVP Project**: No

## Statistics

- **Stars**: 0
- **Forks**: 0
- **Created**: 2026-03-26
- **Last Updated**: 2026-03-26

## Categories & Tags

**Categories**: Uncategorized

**Tags**: None

## README


.. image:: https://travis-ci.org/sonofeft/RocketProps.svg?branch=master

.. image:: https://img.shields.io/pypi/v/RocketProps.svg
        
.. image:: https://img.shields.io/pypi/pyversions/rocketprops

.. image:: https://img.shields.io/pypi/l/RocketProps.svg


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 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.