IMU-P4
Space Inventor ApS
Compact, rugged inertial measurement unit with redundant gyroscopes, accelerometers and magnetometers.
Technical specifications
- MSRP
- €6,000
- Gyroscope/accelerometer
- Two redundant Murata SCH16T-K01 6-DOF XYZ-axis units
- Magnetometer
- Two RM3100 magnetometers
- Interface
- Two redundant microcontrollers, redundant CAN bus with CSP
About
The IMU-P4 is a compact and rugged inertial measurement unit comprising two redundant Murata SCH16T-K01 6-DOF XYZ-axis gyroscope and XYZ-axis accelerometer units, and two RM3100 magnetometers, as well as temperature sensors. The two redundant sets of sensors are interfaced via two redundant microcontrollers and redundant CAN bus interfaces with CSP (CubeSat Space Protocol), making them accessible from the satellite communication bus.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
