About the Project

Northern Arizona University's Active Rocket Controls Team 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.

Mechanical Engineers

Northern Arizona University's Mechanical Engineering Team designs the physical hardware for the Active Rocket Controls system. Their work focuses on creating a durable fin-actuation mechanism and internal structure that support stable flight and withstand launch conditions. The goal is to ensure all mechanical components integrate smoothly with the control electronics and operate reliably during ascent.

Electrical Engineers

Northern Arizona University's Electrical Engineering Team develops the sensors and electronics that enable closed-loop stabilization for the Active Rocket Controls system. They integrate the IMU, flight computer, and actuator drivers into a reliable control unit capable of running rapid feedback loops. The goal is to deliver accurate telemetry and consistent control signals throughout the launch sequence.