88 satellite platforms, components and ground equipment from manufacturers worldwide.
Minimal 6U CubeSat platform with maximum payload volume. PSS with battery, UHF transceiver, electromagnetic detumbling only — no…
6U CubeSat platform with 3-axis ADCS. Up to 12 kg S/C mass, 78 Wh battery, 35 W solar…
GaAs solar panel with built-in electromagnetic coil for CubeSat side surfaces. 98×82.6 mm, 28% efficiency, 480–520 mA Isc,…
GaAs solar panel with integrated electromagnetic coil for CubeSat top/bottom edges. 98×98 mm, 28% efficiency, 480–520 mA Isc,…
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.
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