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A Python Turbomachinery design library for liquid rocket engine applications.

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EliasAoubala/turboRocket

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TurboRocket

A python library for the design and development of turbomachinery in rocket applications.

Background

TurboRocket is a python library enabling the design of turbomachinery components for liquid rocket propulsion systems.

The main goal of this project is to create a set of tools that can be used by designers to create simplified models to assess turbomachinery performance.

Installation

Use the package manager pip to install the TurboRocket library.

pip install turboRocket

Usage

# Need to fill this out at somepoint describing an example use case for the turboRocket library.

Contributing

Pull requests are more than welcome. If major changes are intended, please open an issue thread to discuss the change.

As of current, github issues are being internally used to develop core functionality of the library.

Acknowledgments

Key contributors to this library are:

  • Elias Aoubala (EliasAoubala)
  • Craig Orrock

License

MIT

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A Python Turbomachinery design library for liquid rocket engine applications.

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