Northern Arizona University's Mechanical Engineering Team for Active Rocket Controls is developing a model rocket equipped with a closed-loop stabilization and data acquisition system. The goal is to create a controllable flight platform that can autonomously maintain vertical orientation during powered ascent and collect accurate telemetry throughout the launch sequence.
Our design follows Tripoli Rocketry Association safety standards and incorporates mechanical, electrical, and software subsystems integrated into a modular payload bay. Each subsystem is designed to meet specific engineering requirements, including structural durability, control responsiveness under 50 ms loop timing, and reliable data transmission.