ADCS-R3

Overview
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.
Overview
- Name
- ADCS-R3
- Vendor
- Space Inventor
- Subsystem
- ACDS Subsystem
- Component Type
- ACS/ACDS System
- Form Factor
- CubeSat
- Heritage
- Yes
- Average Cost
- $58,570 USD
- Fiscal Year
- 2021
Vendor Details
- Name
- Space Inventor
- Website
- https://space-inventor.com/
Vendor Request for Information Form
Specifications
- Subsystem
- ACDS Subsystem
- Component Type
- ACS/ACDS System
- Form Factor
- CubeSat
- Vendor
- Space Inventor
- Dry Mass
- 0.6 kg
- Average Power
- N/A
- Heritage
- Yes
- Status
- In Production

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