Key highlights

The TensorCMG Series features variable-speed, single-gimbal CMGs driven by spherical motor technology, available in single and clustered configurations for satellites from 30 kg to 1000 kg.

This spherical motor design reduces weight, volume, and power consumption (SWaP).

An autonomous torque calculation algorithm is integrated on the control board, enabling multi-axis torque output through simple commands.

Applications

  • Earth Observation: The system's fine-pointing capabilities enable high-precision imaging and data collection of Earth's surface.
  • Precise Maneuvering: The TensorCMG facilitates accurate satellite orientation adjustments, essential for tasks such as target tracking and alignment with communication links.
  • Autonomous Operations: With embedded attitude determination and control algorithms, the system supports autonomous modes like sun pointing, detumbling, and safe mode, reducing the need for extensive ground intervention. 

Key features

  • Torque-to-power ratio optimization
  • Form factor: fits tuna-can standard
  • Soft error and hard error fault detection
  • Jitter (micro-vibration): ISO1940 G0.4 @ 8000rpm
  • Magnetic leakage flux shielded with Ni-iron alloy
  • Momentum1 Nms
  • Torque> 3 Nm
  • Gimbal axis angular rangeUnlimited
  • Gimbal Manuever> 30 million
  • Dimensions100 x 100 x 120 mm3
  • Mass< 2.5 kg
  • Rotor ImbalanceISO 1940. G0.4
  • Power @ 0.5 Full, No Torque Output Momentum< 5 W
  • Power @ Max. Momentum, No Torque Output< 9 W
  • Power @ Max. Momentum, Max. Output Torque< 10 W
  • Supplied DC bus Voltage22 ~ 34 V
  • Communication InterfaceRS-422
  • Radiation Hardness> 24 krad(Si) on electronics

Customization

Available in:

  • Standalone version
  • Integrated with other Tensor Tech ADCS components (see TensorADCS integrated product line)
  • With multiple CMGs in a dual, pyramid or rooftop configuration

Flight heritage

The Tensor Tech TensorCMG product line has achieved flight heritage in 2022.

Manufacturing

IPC Class 3 Production and Assembly

Testing & qualification

Environmental Test Following NASA GEVS

Export control

ITAR-Free

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Last updated: 2026-03-11

TensorCMG - Control Moment Gyroscope - Small Sat Series

9TRL

lead time: 26 wk

Downloads

Technical specs

mass
2 to 12 kg
torque
3 to 30 N m
maximum momentum storage
0.2 to 10 N m s

Export

  • Click here to add the Tensor Tech - TensorCMG - Control Moment Gyroscope - Small Sat Series to the Valispace engineering tool from satsearch
  • Click here to add the Tensor Tech - TensorCMG - Control Moment Gyroscope - Small Sat Series to Lynapse Studio by Spacebackend
  • Click here to add the Tensor Tech - TensorCMG - Control Moment Gyroscope - Small Sat Series to 360 by IENAI

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