Projects

Split Hopkinson Pressure Bar (SHPB) Firing System Redesign

Redesigned the SHPB firing mechanism and validated pressure tolerances across critical components to ensure safe, consistent launches.

RPL Project Daedalus

Conducted FEA, CFD, and avionics integration for a high-performance solid rocket system.

High-Impact Containment Enclosure Box

Engineered a polycarbonate enclosure to safely contain debris during dynamic testing

Arduino-Based Remote Controller & Live Sensor

Developed a failsafe control system for real-time pressure and voltage sensor