TensorADCS-20m
3-axis discrete CMG-based ADCS for nanosatellites up to 30 kg with 11.7 mNms momentum capacity.
Technical specifications
- Pointing Knowledge
- 3 ~ 100 arcsec with star tracker; 0.3 deg standard config.
- Max. Momentum
- 11.7 mNms 3-axis
- Slew Rate
- < 5 deg/s
- Control Accuracy
- 0.1 deg
- Torque (Acceleration)
- 1 mNm
- Torque (Gyroscopic)
- 15 ~ 100 mNm
- Dimensions
- Discrete package, see ICD for details
- Nominal Voltage
- 6 ~ 14 V
- Optional Accessories
- GNSS Receiver and Star Tracker
- Mass
- 850 g
- Power
- < 4.2 W
- Interface
- RS-485 or UART
About
The TensorADCS series provides attitude determination and control systems for nanosatellites up to 30 kg, incorporating variable-speed, single-gimbal Control Moment Gyroscopes (CMGs) for 3-axis attitude control and maneuvering, in configurations from 3U to 16U. The TensorADCS-20m is a discrete configuration, with CMG, controller, and sensors installed separately within the satellite structure for flexible component positioning in non-standard layouts, occupying 0.75U total. Same operating modes as the family: Basic (Sun Pointing, Detumbling, Safe Mode) and Advanced/CMG-enabled (Target Tracking, Fine Pointing, Local-Vertical-Local-Horizontal).
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.