CubeSat GaAs Side Solar Panel SXC-SGS-03
SPUTNIXGaAs solar panel with built-in electromagnetic coil for CubeSat side surfaces. 98×82.6 mm, 28% efficiency, 480–520 mA Isc,…
5746 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
GaAs solar panel with built-in electromagnetic coil for CubeSat side surfaces. 98×82.6 mm, 28% efficiency, 480–520 mA Isc,…
6U CubeSat platform with 3-axis ADCS. Up to 12 kg S/C mass, 78 Wh battery, 35 W solar…
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…
NanoAvionics' largest microsatellite platform. 24" ESPA ring, up to 100 kg payload, 200 kg S/C mass, 240 W…
NanoAvionics' smallest microsatellite platform. 11" ESPA ring, up to 25 kg payload, 75 kg S/C mass, 100 W…
16U CubeSat platform for Earth observation, communications, national security, and quantum key distribution. Up to 25 W payload…
15" ESPA-class microsatellite platform. Up to 70 kg payload, 150 kg S/C mass, 164 W payload power, 200…
12U CubeSat platform with double deployable solar panels. Up to 33 W payload power, 18 kg payload mass,…
8U CubeSat platform with deployable solar panels. Up to 29.5 W payload power, 80 Mbps downlink, star-tracker pointing…
6U CubeSat platform in Light, Mid, and Max configurations. Up to 80 Mbps downlink, 12.5–17.5 W payload power,…
Redundant-coil magnetorquer for microsatellite detumbling and magnetic attitude control. Dual-coil dipole up to 5 Am², integrated temperature sensor,…
PC-104 form factor magnetorquer for CubeSat detumbling and magnetic attitude control. Dipole moment up to 0.34 Am², 205…
Single reaction wheel (RW0) or integrated 4-wheel pyramid system (4RW0) for CubeSat 3-axis attitude control. DC brushless motors…
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