Torque Rods
Gimbal Space- ConfigurationCustom solutions available
- SizesMultiple sizes
Custom magnetorquer rods for satellite attitude control, available in multiple sizes — reaction-wheel desaturation and fine attitude control…
15 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Custom magnetorquer rods for satellite attitude control, available in multiple sizes — reaction-wheel desaturation and fine attitude control…
Magnetic torque actuators using alloy cores and bifilar winding for attitude control and momentum dumping — >7,000 units…
Compact three-axis magnetorquer for 6U CubeSats and larger satellites.
Compact 3-axis magnetorquer for 6U CubeSats, combining one air-torquer with two magnetorquer rods.
Series of 7 magnetic torquers for microsatellite attitude control and detumbling. Dipole moments from 1 to 30 Am²,…
Redundant-coil magnetorquer for microsatellite detumbling and magnetic attitude control. Dual-coil dipole up to 5 Am², integrated temperature sensor,…
PC-104 form factor magnetorquer for CubeSat detumbling and magnetic attitude control. Dipole moment up to 0.34 Am², 205…
3-axis magnetorquer for CubeSats, air-torquer + 2 magnetorquer rods, 0.4-0.5 Am² dipole moment, 91x97x17mm, 180g, flight-proven.
Demisable magnetorquer with ±400 A·m² magnetic dipole for attitude control and wheel offloading on medium/large spacecraft. 950 ×…
Demisable magnetorquer with ±140 A·m² magnetic dipole for attitude control and reaction wheel offloading on small/medium spacecraft. Flight…
Compact 3-axis magnetorquer for 6U CubeSats with high torque and low residual dipole, designed to pair with NanoTorque…
At CubeSpace (CS) our extensive range of space-proven magnetic torquers are built using automated machinery and go through…
With only 7.5 grams and 3.2 millimeters thickness, the MT01 Compact Magnetorquer is a vacuum core magnetic coil…
Magnetorquers offer a method of controlling the attitude of a spacecraft. This can be achieved either directly, by…
Magnetorquers offer a method of controlling the attitude of a spacecraft. This can be achieved either directly, by…
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