The propulsion subteam is responsible for developing the engine, tanks, fuel lines, and other propulsion components of the rocket.

01/29/19: Initial CAD model of our optimized rocket nozzle. Next step is to model the cooling channels which make up the nozzle walls.

12/03/18: A screenshot from our Matlab code which we are using to simulate our rocket's trajectory at given inputs for Specific Impulse, Thrust and Mass.