This is the liquid rocket engine parameter solver Alpha release 1 which is the first version for this project. This first version will help to find thrust values by giving some values to the system

Features

  • Calculation of the thrust values (Alpha Release 1)

Project Samples

Project Activity

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Categories

Simulation, Physics

License

Other License

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Additional Project Details

Operating Systems

Linux, Windows

Intended Audience

Aerospace, Quality Engineers, Other Audience, Engineering

User Interface

Win32 (MS Windows)

Programming Language

Python

Related Categories

Python Simulation Software, Python Physics Software

Registered

2023-11-13