nanoST
Solar MEMS TechnologiesCompact plug-and-play star tracker for nanosatellites with <40 arcsec XY accuracy and 15° field of view.
404 satellite platforms, components and ground equipment from manufacturers worldwide.
Compact plug-and-play star tracker for nanosatellites with <40 arcsec XY accuracy and 15° field of view.
Quad-thermopile horizon sensor for nadir vector determination and attitude control on nanosatellites and microsatellites.
MEMS-based digital sun sensor on a chip that measures the two-axis incidence angle of sunlight for accurate sun-tracking…
MEMS-based analog fine sun sensor with ±60° FOV, calibrated with look-up table, for high-accuracy attitude determination.
A two-axis, low-cost digital sun sensor on a chip for high-accuracy sun-tracking, pointing, and attitude determination on nanosatellite…
Two-axis MEMS-based analog sun sensor for CubeSats and nanosatellites with ±60° field of view.
ASTER Labs develops CubeSat nanosatellite systems and payloads, with specialization in deep space navigation using X-ray pulsar timing…
ASPINA offers a lineup of reaction wheels (RWs) designed for small satellite constellations in Low Earth Orbit (LEO),…
Multi-constellation military GNSS receiver with <5 ns timing accuracy, anti-jamming/anti-spoofing, and RAIM for C5ISR and land/air platforms.
NewSpace multi-constellation GNSS receiver for CubeSat and small satellite position, navigation, and timing applications.
Pumpkin's flight GNSS receiver module for CubeSats, built around a NovAtel OEM719-series 555-channel space-grade receiver with dual selectable…
Passive thermo-optical Coarse Earth and Sun Sensor providing spacecraft attitude information during de-spin and safe mode.
SSTL offers highly regarded Space GNSS receivers for satellite navigation and position, velocity, and time information, alongside pioneering…
Space GNSS receiver for small to larger satellites, successor to SGR-10, with multi-GNSS and dual-frequency options.
The SSW-110 is a reaction wheel specifically designed for Low Earth Orbit (LEO) flight, providing attitude control for…
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…
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