Products

Large reusable stainless-steel LOX/LCH4 launch vehicle; 4.5 m diameter, 76.6 m length, 900 t takeoff thrust; vertical landing first-stage recovery.

Proprietary space weather sensor payload integrating a spectrometer and Cherenkov detector, deployed aboard partner satellites in LEO to measure charged particles and geomagnetic conditions.

Mission simulation and design software

Satellite operations software

Orbital transfer vehicle for GTO-to-GEO transfers, 140 kg payload capacity, first launch planned 2028

Orbital transfer vehicle for last-mile satellite delivery in LEO, 200 kg payload capacity, 500 m/s delta-V

150W Hall-effect thruster for microsatellites, 7 mN thrust, up to 60 kNs total impulse

400W Hall-effect thruster for small satellite constellations, 12-32 mN thrust, xenon and krypton

60W Hall-effect thruster for cubesats and nanosatellites (10-80 kg), 2.5 mN thrust, xenon propellant

Modular, scalable space-rated robotic arm system for on-orbit assembly, satellite servicing, and planetary exploration