5615 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Flight-proven ammonia CPS for orbit/attitude correction and flywheel momentum dump (5000–5500 N·s total impulse, 0.02–0.8 N thrust, ≤17…
Flight-proven cold-gas thruster (0.73–0.82 N He/N2, 0.105 kg, 80,000 starts) for precise spacecraft attitude control, flown on KOSMOS…
Consists of two units: Stationary Plasma Thruster with a nominal discharge power of 1350 W and Xenon Flow…
Corrective propulsion system (CPS) consists of a monoblock, including an AIPD-95 CPS engine, a BPU-150 device, a set…
The corrective propulsion system of the UD-AIPD consists of a monoblock, including the KNE block, the BIR1, BIR2…
Dual operating mode: 1.35 / 2.5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical…
Propulsive burn formation for center of mass velocity variation during spacecraft orbit control and braking.
Propellant - hydrazine. The unit consists of two modified thermocatalytic low thrusters: 1 – main, and 1 –…
Propellant - hydrazine. The unit consists of two thermocatalytic low thrusters: 1 – main, and 1 – redundant.…
Flight-proven UDMH/NTO bipropellant low-thrust rocket engine for spacecraft attitude control and orbit correction.
Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands. Design features:…
Flight-proven 13.3 N UDMH/NTO thruster (0.55 kg, 450,000 starts, Isp 2688 m/s) flown on MIR, ISS Zarya module,…
Ultra-lightweight (40 g) flight-proven solenoid valve (0.6 mm, 3.43 MPa, 500,000 cycles) for liquid/gas propellant flow control.
Flight-proven solenoid valve (2.8 mm, 3.0 MPa, 30,000 cycles, 180 g) for high-flow liquid and gaseous propellant control.
Flight-proven solenoid valve (2.2 mm, 2.94 MPa, 60,000 cycles, 180 g) for high-flow propellant control.
Flight-proven solenoid valve (1.8 mm, 2.94 MPa, 310,000 cycles, 180 g) for propellant flow control.
Flight-proven xenon feed unit regulating 1.5–17 mg/s at 1.75 ± 0.1 kgf/cm² for orbit control electric thrusters, 2.6…
Flight-proven xenon feed unit regulating 4–15 mg/s at 2.6 ± 0.12 kgf/cm² for orbit control electric thrusters, 2.6…
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