This ongoing project centers on the design, testing, and launch of a 350 lbf thrust nitrous/IPA bipropellant rocket engine. Working with a small team, I lead the testing effort—developing the structural test stand in CAD and validating it through hand calculations, building the electronics and data ...

Redesigned and rebuilt the test stand fluid panel for Taurus hybrid engine hotfire campaigns. Owned the full system lifecycle, including CAD modeling, component selection, routing, valve specification, and integration for high-pressure nitrous and nitrogen lines. Developed test procedures, coordinat...

Spearheaded the design and assembly of an experimental testing chamber to evaluate and certify Infinitum motors for IP65 compliance. This involved the use of Solidworks to design the system, as well as strict adherence to IP standards, and hands on tool use in the final assembly.

Designed a shuttle valve to meet strict performance requirements: neutral pressure of 700 psia, shuttle pressure of 900 ± 100 psia, and a target CdA range of 1×10⁻³ – 3×10⁻² in² using nitrogen as the working fluid. The objective was to create a functional, manufacturable valve concept through both a...