Propulsion — Space Hardware Marketplace

Bipropellant Low Thrust Rocket Engine

• Year of release1996
• Flight qualification of the productLetter "O1", flight use
• Possibility to adapt the product to customer requirementsYes

A bipropellant low-thrust rocket engine, flight-qualified and adaptable to customer requirements, released in 1996.

Bipropellant Thruster 11d

The Bipropellant Thruster 11d is a flight-qualified propulsion unit designed for spacecraft attitude control, utilizing UDMH/NTO propellants.

Bipropellant Thruster 17D

Flight-proven 13.3 N UDMH/NTO thruster (0.55 kg, 450,000 starts, Isp 2688 m/s) flown on MIR, ISS Zarya module,…

Solenoid Valves 12 PT

The Solenoid Valves 12 PT are single-stage, multi-starting, normally closed valves with a Teflon seal, designed for remote…

Solenoid Valves 26 RT-200

The 26 РТ-200 Solenoid Valve is a single-stage, multi-starting, normally closed valve with a Teflon seal, designed for…

Solenoid Valves RT 200-00-01

The Solenoid Valves РТ 200-00-01 are single-stage, multi-starting, normally closed valves with a teflon seal, designed for remote…

Solenoid Valves RT 200-00-02-03

The Solenoid Valve RT 200-00-02-03 is a single-stage, multi-starting, normally closed valve with a Teflon seal, designed for…

Xenon Feed Unit. Type 1

The Xenon Feed Unit Type 1 provides xenon propellant at specified pressure and flow rate to orbit control…

Xenon Feed Unit. Type 2

The Xenon Feed Unit. Type 2 is a pneumatic automation equipment designed to supply xenon propellant at specified…

3TU Thruster Unit

The 3TU Thruster Unit is a hydrazine-fueled propulsion system designed for spacecraft orientation and attitude control, featuring eight…

Pressure Alarm

A pressure alarm designed to generate an alarm signal when overpressure exceeds the maximum permissible level, suitable for…

Pressure Reducer. Type 1

The Type 1 Pressure Reducer is a pneumatic automation component designed for propellant pressure reduction in spacecraft, offering…

Pressure Reducer. Type 2

The Pressure Reducer Type 2 is a pneumatic automation equipment designed for propellant pressure reduction in spacecraft propulsion…

Pressure Reducer. Type 3 (for pressure integrity check unit)

A Type 3 pressure reducer designed for propellant pressure reduction, suitable for use in pressure integrity check units.

Pressure Reducing Electric Valve

An electric valve designed to open, close, and reduce high-pressure gas lines, maintaining a specified low pressure range.

Solenoid Valves 12 PT-01

The Solenoid Valves 12 PT-01 are single-stage, multi-starting, normally closed valves with a Teflon seal, designed for remote…

Attitude Control Propulsion Unit

The Attitude Control Propulsion Unit is a xenon-fueled propulsion system designed for generating steering effort in spacecraft attitude…

EJK Solenoid Valve

The EJK Solenoid Valve is a single-stage, multi-starting, normally closed, single-seat, teflon seal valve designed for remote flow…