MAI-400

Vendor profile
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”.

Looking for more information or want to purchase?

Contact now

Overview

Name
MAI-400
Vendor
Adcole Maryland Aerospace
Subsystem
ACDS Subsystem
Component Type
ACS/ACDS System
Form Factor
CubeSat
Heritage
Yes

Vendor Details

Name
Adcole Maryland Aerospace
Website
https://adcolespace.com/
Founded
2002

Vendor Request for Information Form

Max. 1000 characters

Please include a detailed description in your message. This helps vendors to better understand your request.

Specifications

Subsystem
ACDS Subsystem
Component Type
ACS/ACDS System
Form Factor
CubeSat
Vendor
Adcole Maryland Aerospace
Dry Mass
0.694 kg
Average Power
1.1 W
Heritage
Yes
Status
In Production
Datasheet
  • Designer logo

    Try Designer

    Design, model, and evaluate satellite mission concepts quickly with our software.

    Launch designer

  • Adcole Maryland Aerospace

    View all products

    • Similar Components

    MAI-25

    Adcole Maryland Aerospace

    MAI-500

    Adcole Maryland Aerospace

    Arcus ADCS

    CubeSat Pointing

    iACS200-1.5

    Hyperion Technologies