24 satellite platforms, components and ground equipment from manufacturers worldwide.
Series of 7 magnetic torquers for microsatellite attitude control and detumbling. Dipole moments from 1 to 30 Am²,…
3-axis magnetometer for microsatellite ADCS. Anisotropic magnetoresistive sensors, ±100,000 nT range, 100 nT noise, 54×52×16 mm, 70 g,…
Sun sensor for microsatellites and small spacecraft. Half-angle 45° FOV, 0.15° accuracy, 43×43×16 mm, 45 g, CAN2B. Uses…
Two-axis digital sun sensor for nanosatellites. ±60° FOV, <0.3° accuracy, 31.3×27.5×10.3 mm, 7 g, CAN interface. Factory calibrated,…
Control flywheel motor (CFM) for microsatellites. Max torque 0.05 Nm, max kinetic moment 2 Nms, 3.2 kg, CAN2B…
A dual-redundant attitude control and stabilization system control unit (OSSCU, SX-SBOX-ADCU-01) running SPUTNIX's flight-qualified ADCS software.
A control flywheel motor (CFM, SX-SBOX-RWH-50-2.0-01) generating control torque via rotor acceleration/deceleration for larger satellite platforms.
A family of proprietary magnetic torquer rods (SX-MT-1 through SX-MT-30) used with the magnetic torquers control unit for…
A control unit (SX-SBOX-MTQU-01) driving up to three magnetic torquers via PDM channels to implement angular velocity damping…
A triaxial anisotropic-magnetoresistive magnetometer (SX-SBOX-MAG-01) used in attitude determination alongside magnetic torquers for detumbling and momentum unloading.
A compact sun sensor (SX-SBOX-SUNS-01) for the attitude control loop, with algorithms mitigating Earth-albedo glare, suitable for microsatellites…
A GNSS receiver unit (SX-SBOX-GNSS-01) providing precision position, velocity and time synchronization for the spacecraft.
A high-precision fibre-optic gyroscope (FOG, SX-SBOX-AVS-FOG-01) with a control unit and 4-element sensitive assembly (3 main + 1…
A triaxial MEMS-based angular velocity sensor (SX-SBOX-AVS-MEMS-01) for small satellite attitude determination.
A 4-flywheel reaction wheel module (SXC-FW4-02) for CubeSat 3-axis attitude control, integrating drivers and control electronics on a…
A compact, ultra-low-power two-axis digital CubeSat sun sensor (SXC-SD-01-3U) with factory calibration and CAN interface.
A passive printed L1-band antenna (AFS-GNSS) for receiving GNSS positioning signals aboard a spacecraft.
Attitude-control actuators of the SX-SBOX suite for microsatellite platforms: ADCS control unit, reaction wheel, magnetorquers and a magnetorquer…
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