GomSpace NanoTorque GST-600 Mk2
GomSpace- Dipole Moment (Z-axis)0.5 Am² (typical)
- Dipole Moment (X/Y-axis)0.4 Am² (typical)
- Dimensions91 x 97 x 17 mm
Compact 3-axis magnetorquer for 6U CubeSats, combining one air-torquer with two magnetorquer rods.
5746 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Compact 3-axis magnetorquer for 6U CubeSats, combining one air-torquer with two magnetorquer rods.
Flight-proven compact low-noise magnetometer with I2C interface for nanosatellites.
Ultra-compact, low power vector sun sensor with I2C interface for CubeSats.
Set of four compact, high-performance reaction wheels qualified for 5 years in-orbit operation.
Modular lithium-ion battery family from Airbus designed for LEO constellation satellites, using automotive-grade cells.
State-of-the-art modular PCDU for Earth observation, science and interplanetary satellite missions.
Compact, low-power avionics unit integrating on-board computing, TM/TC, GPS receiver and AOCS interfaces for 10-year LEO missions.
Compact solid-state mass memory recorder providing high-end onboard data storage for Earth observation missions.
Fully qualified off-the-shelf power supply regulator handling up to 23 kW at 50V for telecom satellites.
Compact, lightweight PCDU delivering up to 1.5 kW of unregulated power for New Space satellite platforms.
Family of high-reliability fibre-optic gyroscopes providing precision inertial attitude sensing for LEO to deep-space missions.
Three-axis fibre-optic inertial unit from the ASTRIX 1000 series offering low angular random walk and optional accelerometer channels…
High-conductance flexible thermal straps for mechanically decoupled heat transport on spacecraft.
High-torque control moment gyroscope for large satellites up to 3 tonnes, featuring a compact patented design.
Power processing unit that conditions and controls power for Hall-effect electric propulsion thrusters.
Compact New Space power processing unit for satellite electric propulsion with a 10-year LEO lifetime.
Compact control moment gyroscope for agile attitude control of small-to-medium satellites up to 1 tonne.
Mid-class control moment gyroscope with integrated micro-vibration dampers for 1-2 tonne satellites.
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