Chemical Propulsion — Space Hardware Marketplace

Station Keeping Thruster Unit Based on Modified Thermocatalytic Thrusters

A thermocatalytic thruster unit designed for spacecraft station keeping, utilizing hydrazine propellant and featuring redundant components for reliability.

Station Keeping Thruster Unit Based on Thermocatalytic Thrusters

A thermocatalytic thruster unit designed for spacecraft station keeping, utilizing hydrazine propellant and featuring main and redundant thrusters,…

Modified Thermocatalytic Low Thruster

A hydrazine monopropellant thermocatalytic thruster used for spacecraft orientation, attitude control, and station keeping, with flight-qualified heritage on…

Modified Thermocatalytic Thrusters

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…

Pressure Stabilization Unit

The Pressure Stabilization Unit (PSU) is a flight-qualified component designed to maintain stable propellant pressure for spacecraft propulsion…

Attitude Control Thruster Unit Based on Modified Thermocatalytic Low Thrusters

A spacecraft attitude control thruster unit utilizing two modified thermocatalytic low thrusters, designed for orientation and attitude adjustments.

Attitude Control Thruster Unit Based on Thermocatalytic Low Thrusters

A thermocatalytic low thruster unit designed for spacecraft orientation and attitude control, using hydrazine propellant.

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,…

3TU Thruster Unit

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

Working Medium Tank MVSK

The Working Medium Tank MVSK is a monopropellant propulsion system designed for spacecraft, storing and feeding hydrazine to…

Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm)

A monopropellant tank with a stiff-plastic separation device (diaphragm) designed for spacecraft propulsion systems, capable of storing and…

MULTI-LAYER BELLOWS

Multi-layer bellows designed for use as sensing elements, phase separators, sealing devices, and power unit components in various…

Bipropellant Tank with Stiff-Plastic Separation Devices (Diaphragms)

A bipropellant tank with stiff-plastic separation devices (diaphragms) designed for the KDU 11D414HC propulsion system of communication satellites,…