Avionics (Teknofest Rocket Competetion)

For the Teknofest International Rocket Competition, we developed a dual-redundant avionics system for a sounding rocket. The objective was to build a flight computer capable of logging sensor + GPS data, detecting apogee autonomously triggering parachute deployment (pyro activation), and sending telemetry to the ground station.

Project Overview

Hardware Architecture (Primary Flight Computer)

Diagrams

Schematic of Avionics
Pcb Layout of Avionics (Front Side)
Pcb Layout of Avionics (Back Side)
Manufactured PCB
Assembled board with components installed

My Learnings