ADCS-R3

Search
Generic filters
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
Vendor Request for Information Form

    Name *

    Email *

    Country *

    Would you like suggestions about similar products/services from other suppliers?

    Inquiry Description *

    SPECIFICATIONS
    SubsystemACDS
    ClassificationIntegrated Attitude System
    Form FactorCubeSat
    VendorSpace Inventor
    HeritageN/A
    Mass0.6 kg

    Resources