# RocketIsp

**Repository Path**: openminds/RocketIsp

## Basic Information

- **Project Name**: RocketIsp
- **Description**: Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.
- **Primary Language**: Unknown
- **License**: GPL-3.0
- **Default Branch**: master
- **Homepage**: None
- **GVP Project**: No

## Statistics

- **Stars**: 0
- **Forks**: 0
- **Created**: 2026-03-28
- **Last Updated**: 2026-03-28

## Categories & Tags

**Categories**: Uncategorized

**Tags**: None

## README



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

.. image:: https://img.shields.io/pypi/v/RocketIsp.svg
        
.. image:: https://img.shields.io/badge/python-3.5|3.6|3.7|3.8-blue

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


RocketIsp is in the early stages of development... should stabilize soon.

**Rocketisp** Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.


See the Code at: `<https://github.com/sonofeft/RocketIsp>`_

See the Docs at: `<http://rocketisp.readthedocs.org/en/latest/>`_

See PyPI page at:`<https://pypi.python.org/pypi/rocketisp>`_



**Rocketisp** uses a simplified JANNAF approach to calculate delivered
specific impulse (Isp) for liquid rocket thrust chambers.

Note that **RocketIsp** gets propellant properties from the companion project `RocketProps <https://rocketprops.readthedocs.io/en/latest/>`_
and ideal Isp performance from the companion project  `RocketCEA <https://rocketcea.readthedocs.io/en/latest/>`_ .