| Introduction |
1. Rocket-based Fixed-Wing UAV : A foldable fixed-wing unmanned aerial vehicle based on a solid-fuel rocket for reaching the lower stratosphere at an altitude of 30 km
2. Propulsion System for Satellite Attitude Control and Orbital Transfer : A thruster using solid propellant that enables ignition, reignition, extinguishing, and thrust control through electrical energy regulation. This propulsion system, designed for precise satellite attitude control and orbital transfer, offers advantages over liquid thrusters due to the lighter weight and higher space efficiency of the solid propellant.
3. Satellite attitude control simulation device using a robotic arm : A device that simulates the dynamics of an satellite by attaching a dummy satellite and a sensor to the end-effect of the robotic arm to analyze the dynamics of the satellite. |
Exhibition > Online Exhibition
