Planetary Probe Descent Simulation CanSat

Designed a CanSat to simulate the landing sequence of a planetary probe using multi-phase descent: parachute deployment, heat shield aerobraking, and post-landing actuation. The mission required the CanSat to be launched to 670-725 meters altitude and survive violent deployment forces. The system utilized a three-stage descent: initial parachute descent at 15 m/s, heat shield aerobraking at 20 m/s or less from 500m, and final parachute deployment at 5 m/s from 200m with post-landing flag deployment and video recording.