A 3kN rocket with self-pressurising N₂O and regulated IPA pressurisation, designed, built, and taken through hot-fire testing.
A liquid oxygen pump built with a custom submerged motor to output 3kg/s at 45BarA.
A full kick-stage design for micro-launchers, leading a team of four, spanning propulsion, GNC, structures, and RCS.
Cryogenic fluid systems for engine and stage test stands, spanning commissioning and flight hardware testing.
A test chamber with variable humidity and oxygen control, using an Arduino-based PID system and low-cost lab equipment.
Modifying 25 SM13 compressors to be used in argon recovery while establishing build and test procedures.
Designing a geodesic fibreglass dome to renovate the school's observatory.