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.

"1. Use PE Cluster to make the calculation reconfigurable,can be modularized into 36X PEs, supporting up to 2160PEs 2. It can be configured as an independent IP with high computing throughputlow power consumption. The computing performance can reach 864 GOPS@200MHz when 2160PEs are employed."