MAI-400

MAI-400 image

Overview

This 1/2U (10cm x 10cm x 5.16cm) Attitude Determination and Control System features three reaction wheels, a 3-axis magnetometer, two IR Earth Horizon Sensor (IREHS), three electromagnets 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. It can be placed either at the bottom or the top of a CubeSat stack. It also has cable channels for customer cable “feed-arounds”.

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Overview

Name
MAI-400
Component Type
ACS/ACDS System
Form Factor
CubeSat
Heritage
Yes

Vendor Details

Name
Adcole Maryland Aerospace
Founded
2002

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Specifications

Component Type
ACS/ACDS System
Form Factor
CubeSat
Dry Mass
0.694 kg
Average Power
1.1 W
Heritage
Yes
Status
In Production
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