Satellite Attitude Control Computer, which performs functions including satellite attitude information acquisition, adjustment, and control. It features a standard 3U board card size and is suitable for small satellites weighing 50-200kg. The system is characterized by its lightweight, compact size, low power consumption, and cost-effectiveness.

Utilizing a "passive" spiral spring as the deployment drive, combined with the company's self-developed "damper," can achieve high-precision deployment requirements for a 10m-diameter flat-panel SAR antenna, with a post-deployment frequency of no less than 2Hz.

A fully mechanical damper for controlled slow deployment of passive mechanisms.

The reaction wheel is one of the actuators in a satellite’s attitude control system. When the satellite experiences external disturbance torques, the wheel accelerates or decelerates under command to generate a reaction control torque, absorbing angular momentum changes caused by the disturbances and thereby maintaining stable satellite attitude. A 0.3 N·m·s reaction wheel is typically suitable for satellite platforms weighing 30–100kg.