Calculate Optimal Design of Rocket Propulsion Systems (Kerbal Space Program).

A comprehensive solution for designing and optimizing student-built liquid rocket engines.

liquid rocket engine design, development, and sizing code

Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.

Database of propulsion system components for electric and fuel powered UAVs

A Python Turbomachinery design library for liquid rocket engine applications.

Bench for measuring parameters of propulsion system (propeller, motor, regulator) of unmanned drones