2.5Nms single frame control moment gyroscope
Product Introduction
It is composed of opto-electromechanical components such as high-speed momentum wheels, conductive slip rings, photoelectric encoders, PMSM motors, etc., and realizes the rapid exchange of angular momentum with the spacecraft by changing the angular momentum direction of the constant-speed momentum wheel, so as to improve the maneuvering control ability of the spacecraft.

Suitable for small agile maneuvering satellites
Product Features

High torque (max. 5 Nm)

Low power consumption (steady-state power consumption<17W)

High accuracy (minimum speed<0.005°/s)

Light weight (less than 4.5kg)

Support customized production on demand.

Specification Parameters
  • 产品材质
  • 产品尺寸
  • 中心波长
  • 半峰值带宽
  • 峰值透过率
  • 截止波长
  • 截止深度
  • 表面光洁度