ADCS-R3

Overview

The ADCS-R3 is an integrated attitude control solution for 2-6 kg satellites. It includes four momentum wheels in tetrahedron configuration, three magnetorquer rods, gyro, accelerometer and ADCS computer in a very compact and rugged package. It is designed to operate with external attitude sensors connected via CAN bus such as sun sensors, star trackers and other.

Specifications

Component Type
ACS/ACDS System
Form Factor
CubeSat
Dry Mass
0.6 kg
Average Power
N/A
Heritage
Yes
Status
In Production