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.

A Python Turbomachinery design library for liquid rocket engine applications.

Database of propulsion system components for electric and fuel powered UAVs

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