Designed and validated two coaxial sleeve valves for use on Waterloo Rocketry's 2026 Rocket, Polaris. Increased flow rate through the injector valves by 40% will reducing mass by 60% and simultaneously reducing footprint. Performed stress analysis to ensure reliable operation for fluid pressures u...

Developed piping and instrumentation diagrams for rocket and ground side fluid systems. Authored test procedures for rocket cold flow and hot fire tests. Led testing operations, managing a team of up to 20 personnel.

Designed, manufactured, and validated a rapidly reusable quick-disconnect arm mechanism, controlling the release of oxidizer fill plumbing from the rocket. Implemented a modular design, validated through effective usage in three different configurations.

Spearheaded the design and manufacturing of testing infrastructure for a hotfire test of Waterloo Rocketry's Eridium V2 engine. Performed stress analysis on all components, designing for a peak thrust of 15 kN. Managed a team of 5 other engineers through the manufacturing and assembly of the hardw...