HARDWARE / PRODUCTUpdated 24 Jul 2026

3-Axis Magnetorquer NanoTorque GST-600

GomSpace
3-Axis Magnetorquer NanoTorque GST-600

The NanoTorque GST-600 is a compact three-axis magnetorquer designed for satellite attitude control, suitable for 6U CubeSats and other small satellites.

Typed specifications56 values

Discloses 6 of 8 fields engineers filter by in this category (category median 3).

Magnetic dipole moment
0.4 A·m²
typ. · X- and Y-axis at 20 ℃ · datasheet p.7 0.23 A·m² min · X- and Y-axis at 20 ℃  |  0.34 A·m² min · Z-axis at 20 ℃  |  0.5 A·m² typ. · Z-axis at 20 ℃  |  0.4 A·m² nom. · X- and Y-axis at 20 ℃  +1
Mass
180 g
typ. · datasheet p.8 180 g
Envelope (L×W×H)
90.5 x 96.9 x 17.2
datasheet p.8
Supply voltage
5 V
nom. · recommended PWM voltage amplitude, ± · datasheet p.7 3.6 V max · Maximum supply voltage and logic voltage for TMP100 temperatu…  |  3.3–5.5 V recommended PWM voltage amplitude, ±
Power consumption
0.003 W
typ. · Standby, X- and Y-axis at 20 ℃ · datasheet p.7 0.5 W avg, X- and Y-axis at 20 ℃  |  0.72 W avg, Z-axis at 20 ℃  |  0.5 W Avg. (X- and Y-axis)  |  0.72 W Avg. (Z-axis)  +12
Data interface
I2C
TMP100 sensor · datasheet p.4 I2C TMP100 temperature sensor, address 0x4e  |  I2C
Operating temperature
-35 °C
min · datasheet p.7 70 °C max  |  -35–70 °C
TRL
8
datasheet p.8
Magnetorquer type
rod
datasheet p.4 3-axis torquer board single air-torquer and two magnetorquer-rods
Axes
3
datasheet p.4
Driver electronics
integrated
datasheet p.7 external externally PWM-driven coils
Connector
J1 magnetorquer Z-axis: Molex PicoBlade 53398-0671
datasheet p.5 Molex PicoBlade 53398-0671 J1 - Magnetorquer Z-Axis  |  Molex PicoBlade 53398-0471 J2 - Communication  |  Molex PicoBlade 53398-0471 J3 - Communication  |  Molex PicoLock 503763-0291 J4 - Magnetorquer X-Axis  +3
Survival temperature
-35 °C
min · datasheet p.7 70 °C max  |  -35–70 °C storage
Flight heritage
Flight-proven
product page
Satellite class
CubeSat
designed for 6U CubeSats · datasheet p.4
Coil resistance
39.5 Ω
nom. · X- and Y-axis at 20 ℃ · datasheet p.7 25.5 Ω nom. · Z-axis at 20 ℃

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier7 lines, in the manufacturer's own wording
Dipole moment (Z-axis)
typ. 0.5 Am²
Dipole moment (X/Y-axis)
typ. 0.4 Am²
Temperature sensor
Integrated
Dimensions
91 x 97 x 17 mm
Mass
180 g
Configuration
1 air-torquer + 2 magnetorquer rods
Flight heritage
Flight-proven

About

The NanoTorque GST-600 is a compact three-axis magnetorquer system designed primarily for 6U CubeSats, but adaptable for use in both smaller and larger satellites. It enables precise attitude control by altering the current in its components. The system comprises a single air-torquer and two magnetorquer-rods. Key features include high torque capabilities for effective satellite attitude adjustment and a low residual dipole to minimize interference with sensitive onboard sensors and other equipment. The NanoTorque GST-600 is engineered for seamless integration with the NanoTorque GSW-600 series, forming a compact, reliable, and efficient solution for precise nanosatellite attitude control, ensuring stability and flexibility throughout a mission.

Documentation

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

Source: gomspace.com ↗

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