HARDWARE / PRODUCTUpdated 25 Jul 2026

NanoTorque GST-600

GomSpace
NanoTorque GST-600

A compact three-axis magnetorquer combining a single air-torquer and two magnetorquer-rods for satellite attitude control, designed for 6U CubeSats and scalable to smaller and larger satellites.

Technical specifications

Type
3-axis magnetorquer (1 air-torquer + 2 magnetorquer rods)
Target platform
Primarily 6U CubeSat (also usable in smaller/larger))
Torque
High torque, low residual dipole
Integration
Compatible with NanoTorque GSW-600 reaction wheels
Flight heritage
Flight-proven GomSpace product line
Operating temperature
-35…70 °C
Storage temperature
-35…70 °C
Supply voltage
3.3…5.5 V
Dipole moment (Z-axis)
0.34…0.5 Am2
Dipole moment (X- and Y-axis)
0.23…0.4 Am2
Resistance (Z-axis)
25.5 Ω
Resistance (X- and Y-axis)
39.5 Ω
Temperature coefficient (Z-axis)
0.104 Ω/°C
Temperature coefficient (X- and Y-axis)
0.155 Ω/°C
Power consumption (Z-axis, standby)
3 mW
Power consumption (Z-axis, average)
720 mW
Power consumption (Z-axis, max)
900 mW
Power consumption (X- and Y-axis, standby)
3 mW
Power consumption (X- and Y-axis, average)
500 mW
Power consumption (X- and Y-axis, max)
625 mW
Mass
180 g
Dimensions
90.5 x 96.9 x 17.2 mm

About

The NanoTorque GST-600 is a compact three-axis magnetorquer designed primarily for 6U CubeSats but usable in both smaller and larger satellites. The system consists of a single air-torquer and two magnetorquer-rods. Attitude control of the satellite is achieved by altering the current flowing through the air-torquer and the magnetorquer rods, generating magnetic dipole moments that interact with the Earth’s magnetic field to produce control torques. The product features high torque capabilities, providing the necessary force for adjusting satellite attitude, combined with low residual dipole to minimize interference with sensors and other equipment on board. The 3-axis magnetorquer is designed for seamless integration with the NanoTorque GSW-600 series; when combined, they form a compact, reliable, and efficient integrated attitude control solution for precise nanosatellite attitude control, ensuring stability and flexibility throughout the mission.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: gomspace.com ↗

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