3" McMaster shipping tube rocket to 4000 ft on an Aerotech I366R motor
54mm minimum diameter flight to 7600 ft and Mach 1 on an Aerotech J425R motor
Independent Project | March 2025 - present
Single seperation dual deploy recovery system for a future liquid bipropellant spaceshot vehicle
Space Enterprise at Berkeley | September 2024 - March 2025
Solid propellant ignitor for an 11kN regeneratively-cooled, nitrous-oxide/isopropanol spaceshot rocket engine
Space Enterprise at Berkeley | September 2023 - November 2024
Test stand to static fire an 8.5 kN, P-impulse class experimental solid rocket motor
Space Enterprise at Berkeley | December 2023 - April 2024