Space Hardware Marketplace

High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg

This is a high-powered, multimode electric thruster designed for spacecraft up to 3000 kg, featuring W-Ba emitter cathodes.

Integrated Thruster Unit 13

The Integrated Thruster Unit 13 (ITU) is a propulsion system designed for spacecraft orbit formation and station keeping,…

Integrated Thruster Unit ITU-5000M

The ITU-5000M is an integrated thruster unit designed for spacecraft orbit formation and station keeping, featuring a high-precision…

Electric Thruster for Spacecraft with Mass up to 1500 kg

An electric thruster designed for spacecraft up to 1500 kg, offering high specific impulse at relatively low power…

Electric Thruster for Spacecraft with Mass up to 2500-3000 kg

This is an electric Hall-effect thruster designed for spacecraft with a mass of up to 2500-3000 kg, offering…

Electric Thruster for Spacecraft with Mass up to 3000 kg 1

This is an electric, multimode thruster designed for spacecraft up to 3000 kg, featuring W-Ba emitter cathodes and…

Electric Thruster for Spacecraft with Mass up to 3000 kg

An electric thruster designed for spacecraft up to 3000 kg, featuring high specific impulse and W-Ba emitter-based cathodes.

Cold Ammonia Corrective Propulsion System

A cold-gas ammonia corrective propulsion system (CPS) for correcting and stabilizing spacecraft orbit parameters and zeroing the kinetic…

Cool Gas Thruster

A cool gas thruster designed for precise spacecraft orientation, featuring small size and mass, and capable of generating…

Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit

A Correction Unit (CU) featuring a Stationary Plasma Thruster with 1350 W nominal discharge power and a Xenon…

Corrective Propulsion System 95

The AIPD-95 corrective propulsion system is designed for spacecraft orbit correction and maintenance, featuring a pulsed operating mode…

Corrective Propulsion System UD-AIPD

The UD-AIPD is a corrective propulsion system designed for spacecraft orientation and correction, featuring a monoblock design and…

Dual-mode Stationary Plasma Thruster with a Nominal Discharge Power of 2500/1350 W

A dual-mode stationary plasma thruster with nominal discharge powers of 2500W and 1350W, designed for spacecraft station keeping…

Adjustment and Braking Engine

The Adjustment and Braking Engine is a four-chamber propulsion system designed for unmanned spacecraft reactive control, orbit control,…

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.