5746 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
CubeSat deployment system for launching CubeSat payloads into orbit from host launch vehicles.
Fault-tolerant CubeSat electrical power system combining power distribution, battery management, and solar array conditioning.
Modular UHF/VHF deployable antenna system with triple-redundant deployment for CubeSats from 1U to 16U.
Modular CubeSat structural platform series spanning 1U to 16U with flight-proven reliability and custom interfaces.
High-endurance HPGP monopropellant thruster delivering 5.5-22 N thrust for AOCS and delta-V maneuvers on medium satellites.
High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.
Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.
Green propellant thruster variant delivering 1 N thrust for low-toxicity attitude control and delta-V maneuvers.
Low-toxicity ADN-based HPGP monopropellant thruster delivering 0.1 N thrust for AOCS and small delta-V maneuvers.
Flight-proven HPGP monopropellant thruster delivering 0.25-1 N thrust, used for AOCS and delta-V on CubeSats to smallsats.
Mid-class HPGP monopropellant thruster delivering 1.4-5.5 N thrust for AOCS and delta-V on small and medium satellites.
Analogue quadrant-detector sun sensor providing precise two-axis solar aspect angle for yaw steering and earth-pointing missions.
Compact, lightweight version of the Fine Sun Sensor for small satellites and CubeSats requiring precise sun-vector data.
Self-redundant cosine-response sun sensor delivering reliable wide-angle solar position data for safe-mode operations.
Precision instrument for measuring microgravity acceleration levels aboard crewed and uncrewed spacecraft.
Rugged self-redundant sun sensor delivering coarse solar position data for safe-mode and coarse maneuvering.
Modular small satellite bus supporting up to 250 kg payload in three variants (S, D, DX) for Earth…
High-resolution optical imager achieving 1.9 m GSD with 15 km swath from LEO for Earth observation missions.
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