Powered by hybrid rocket engines designed in-house, the rocket achieves vertical takeoff, hovering, vertical landing,precise attitudetrajectory control using throttle controls as well as thrust vectoring controls. In addition, this rocket includes the following notable technologies: 10ms near hard real-time GNC system, highly modular application-like flight software, 10Hz bandwidth flow control system, 5Hz bandwidth direct-drive motor thrust vectoring system, High Test Peroxide hybrid rocket engine with a vacuum specific impulse of 305 seconds.
