All Purpose Rocket Avionics (APRA) Flight Computer

Designing the APRA Flight Computer for compatibility with a wide range of rocketry projects

Developing a custom printed circuit board integrating an STM32 microcontroller, dual inertial measurement units, barometer, magnetometer, GPS, and Bluetooth module

Implemented 6 servo outputs to enable control functions such as thrust vectoring and active fin control, with flexibility to expand additional functionalities

Integrated 4 pyro channels to reliably trigger flight events including stage separation and parachute deployment