Lead structures team to design robust lightweight UAV fuselage & payload deployment mechanism. Leveraged design skills in Solidworks & manufacturing skills in composite and subtractive manufacturing processes to design ~13 lbs fuselage. Prototyped purely mechanical 2-stage delayed parachute deployment mechanism to land payload inside a 40-foot diameter circle from 80ft+ off the ground with 85% accuracy. Diagnosed vehicle issues during flight testing involving PID tracking, vibration analysis, and autonomous feature testing using PX4 flight review software

Led Kit Based Busbar packaging project to encourage automation in customer assembly lines