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
and ideal Isp performance from the companion project RocketCEA .
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