5195 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…
We use cookies. Strictly necessary cookies keep the platform working. With your consent we also use Google Analytics to understand how the platform is used and improve it. We do not use advertising cookies. Cookie Policy · Privacy
Favorites are available to clients only. Sign in to your client cabinet or create a free account — it takes less than a minute.
How is your experience with the platform? Your message goes straight to our team.
Thank you! Your feedback has been sent to our team.
