539 satellite platforms, components and ground equipment from manufacturers worldwide.
A thermocatalytic low thruster unit designed for spacecraft orientation and attitude control, using hydrazine propellant.
A bipropellant low-thrust rocket engine, flight-qualified and adaptable to customer requirements, released in 1996.
The Bipropellant Thruster 11d is a flight-qualified propulsion unit designed for spacecraft attitude control, utilizing UDMH/NTO propellants.
Flight-proven 13.3 N UDMH/NTO thruster (0.55 kg, 450,000 starts, Isp 2688 m/s) flown on MIR, ISS Zarya module,…
The Solenoid Valves 12 PT are single-stage, multi-starting, normally closed valves with a Teflon seal, designed for remote…
The 26 РТ-200 Solenoid Valve is a single-stage, multi-starting, normally closed valve with a Teflon seal, designed for…
The Solenoid Valves РТ 200-00-01 are single-stage, multi-starting, normally closed valves with a teflon seal, designed for remote…
The Solenoid Valve RT 200-00-02-03 is a single-stage, multi-starting, normally closed valve with a Teflon seal, designed for…
The Xenon Feed Unit Type 1 provides xenon propellant at specified pressure and flow rate to orbit control…
The Xenon Feed Unit. Type 2 is a pneumatic automation equipment designed to supply xenon propellant at specified…
The 3TU Thruster Unit is a hydrazine-fueled propulsion system designed for spacecraft orientation and attitude control, featuring eight…
A pressure alarm designed to generate an alarm signal when overpressure exceeds the maximum permissible level, suitable for…
The Type 1 Pressure Reducer is a pneumatic automation component designed for propellant pressure reduction in spacecraft, offering…
The Pressure Reducer Type 2 is a pneumatic automation equipment designed for propellant pressure reduction in spacecraft propulsion…
A Type 3 pressure reducer designed for propellant pressure reduction, suitable for use in pressure integrity check units.
An electric valve designed to open, close, and reduce high-pressure gas lines, maintaining a specified low pressure range.
The Solenoid Valves 12 PT-01 are single-stage, multi-starting, normally closed valves with a Teflon seal, designed for remote…
The Attitude Control Propulsion Unit is a xenon-fueled propulsion system designed for generating steering effort in spacecraft attitude…
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