Metadata-Version: 2.1
Name: rocketprops
Version: 0.1.7
Summary: RocketProps models liquid rocket propellants.
Home-page: http://rocketprops.readthedocs.org/en/latest/
Download-URL: https://github.com/sonofeft/RocketProps
Author: Charlie Taylor
Author-email: cet@appliedpython.com
License: GPL-3
Keywords: rocketprops setuptools development
Platform: any
Classifier: Development Status :: 4 - Beta
Classifier: Operating System :: OS Independent
Classifier: Intended Audience :: Developers
Classifier: Intended Audience :: End Users/Desktop
Classifier: Topic :: Software Development :: Build Tools
Classifier: License :: OSI Approved :: GNU General Public License v3 (GPLv3)
Classifier: Programming Language :: Python :: 3.6
Classifier: Programming Language :: Python :: 3.7
Classifier: Programming Language :: Python :: 3.8
Classifier: Programming Language :: Python :: 3.9
Classifier: Programming Language :: Python :: 3.10
Classifier: Programming Language :: Python :: 3.11
Description-Content-Type: text/x-rst
Provides-Extra: dev
Provides-Extra: test
License-File: LICENSE.txt
License-File: AUTHORS.rst



.. 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.



