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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Release files for rocketisp 0.1.13
For a detailed explanation of source distributions (sdists) and built distributions (wheels), please see the package formats documentation.
Source distribution (sdist)
| File | Size | Uploaded | |
|---|---|---|---|
| rocketisp-0.1.13.tar.gz | 39.3 MB | Details |
Built distribution (wheel)
| File | Interpreter | ABI | Platform | Reset |
|---|---|---|---|---|
| rocketisp-0.1.13-py2.py3-none-any.whl | Python 3, Python 2 | none | any | Details |
Total release size: 43.0 MB
Release files / rocketisp-0.1.13.tar.gz
| Download URL | rocketisp-0.1.13.tar.gz |
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| Size | 39.3 MB |
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Release files / rocketisp-0.1.13-py2.py3-none-any.whl
| Download URL | rocketisp-0.1.13-py2.py3-none-any.whl |
|---|---|
| Size | 3.6 MB |
| Tags | Python 2 Python 3 |
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