MAI-500

Overview

This 0.6U Attitude Determination and Control System features two Star Trackers, three reaction wheels, three electromagnets, a 3-axis magnetometer, and an ADACS computer for a stand-alone, Plug-and-Play attitude control system for small satellites. The configuration is compatible with the CubeSat standard. The Star Trackers are oriented either 180 or 90 degrees apart and angled upward at 24 degrees. Other mounting angles are available.

Specifications

Component Type
ACS/ACDS System
Form Factor
CubeSat
Dry Mass
1.049 kg
Average Power
2.1 W
Heritage
N/A
Status
In Production
  • Adcole Maryland Aerospace

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