01 — Data Acquisition
DAQ System
Custom data acquisition system for rocket engine test stands. Multi-channel sensor fusion with real-time telemetry and high-speed logging. Designed from schematic to fabricated board and deployed in field testing conditions in the Mojave Desert.
Responsibilities included sensor selection, signal conditioning circuit design, PCB layout in KiCad, embedded firmware in C, and live data visualization during test fires.
02 — Avionics
Flight Controller PCB
Custom avionics board for high-powered rocketry. Features motor drivers, dual telemetry modules, battery management, and an STM32 microcontroller in a compact, flight-ready layout. Designed for SEDS UCSD's liquid-fuel rocket program.
03 — Propulsion
Engine Test Stand
Field instrumentation and operation of a liquid-fuel rocket engine test stand. Responsible for sensor hookup, wiring harnesses, DAQ pipeline, and remote fire control during desert test campaigns. Analyzed thrust curves and combustion stability post-test.