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