Student Self-Landing VTVL Rocket — Avionics

Led early avionics architecture for a student VTVL rocket, coordinating with guidance, propulsion, and mechanical teams to define subsystem responsibilities and electrical interfaces.

Independently designed and laid out a multipurpose STM32 controller PCB with CAN, UART, I²C, and SPI interfaces for propulsion and thrust-vector-control applications; teammates later validated the prototype.

Built a DAQ-based pressure-measurement setup and STM32 valve controller for propellant-feed-system tests, supporting early verification of line pressures and valve actuation.