ADCS-R3

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Description

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.

 

Datasheet

Space Inventor – ADCS-R3

Overview
NameADCS-R3
ManufacturerSpace Inventor
SubsystemACDS
ClassificationIntegrated Attitude System
Form FactorCubeSat
Vendor Overview
Vendor NameSpace Inventor
Vendor Websitehttp://space-inventor.com/
Vendor LocationDenmark
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SPECIFICATIONS
SubsystemACDS
ClassificationIntegrated Attitude System
Form FactorCubeSat
VendorSpace Inventor
HeritageN/A
Mass0.6 kg

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