541 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
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…
Propellant - hydrazine. The unit consists of eight thermocatalytic low thrusters: 4 – main, and 4 – redundant.…
Pneumatic pressure alarm unit generating an overpressure warning signal at 4.5 kgf/cm², 15.6-year active lifetime.
Pneumatic pressure reducer for xenon/propellant feed lines, reducing 250 to 1.75 ± 0.1 kgf/cm², 0.15 kg, 15.5-year lifetime.
Pneumatic pressure reducer for propellant feed lines, reducing 250 to 2.6 ± 0.12 kgf/cm², 0.15 kg, 15.5-year lifetime.
Pneumatic pressure reducer for pressure integrity check units, reducing up to 140 to 1.7 ± 0.17 kgf/cm², 0.15…
Combined high-pressure valve and regulator (350 to 4.5 kgf/cm², 27 V DC, 1.9 kg) for spacecraft gas line…
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