ChallengeOne Reaction Wheel
Attitude-control reaction wheel module for the ChallengeOne satellite platform, part of its Attitude Determination and Control System (ADCS).
Technical specifications
- Input voltage
- 4-15 V
- Communication bus
- 2x CAN2B; Battery UART
- Operating temperature
- -40 to +86 °C
- Storage temperature
- -50 to +105 °C
- Shock resistance
- 50 g
About
The Reaction Wheel provides fine attitude control for the ChallengeOne satellite platform as part of its Attitude Determination and Control System (ADCS), interfacing over dual CAN2B buses plus a battery UART link.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.