Skip to main content

RocketProps models liquid rocket propellants.

Project description

https://travis-ci.org/sonofeft/RocketProps.svg?branch=master https://img.shields.io/pypi/v/RocketProps.svg https://img.shields.io/pypi/pyversions/rocketprops 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.

Project details


Download files

Download the file for your platform. If you're not sure which to choose, learn more about installing packages.

Source Distribution

rocketprops-0.1.7.tar.gz (1.3 MB view hashes)

Uploaded source

Built Distribution

rocketprops-0.1.7-py2.py3-none-any.whl (1.3 MB view hashes)

Uploaded py2 py3

Supported by

AWS AWS Cloud computing and Security Sponsor Datadog Datadog Monitoring Fastly Fastly CDN Google Google Download Analytics Microsoft Microsoft PSF Sponsor Pingdom Pingdom Monitoring Sentry Sentry Error logging StatusPage StatusPage Status page