Space Hardware Marketplace

Inertial Measurement Unit

• PurposeMeasurement of velocity and angle increments on three sensitive axes of fiber-optic gyroscopes and vibrating string accelerometers of measurement channels and transmission of that information to the control system.
• Year of release2015
• Design life15 years

An Inertial Measurement Unit (IMU) designed for future manned spacecraft, providing precise measurement of velocity and angle increments…

Kinetic Moment Reset System 1207

The Kinetic Moment Reset System 1207 is designed to calm low-orbit spacecraft and dissipate accumulated kinetic moment from…

Backup Inertial Measuring Device

• PurposeMeasurement of angular velocities in three axes.
• Year of release2018
• Design life10 years

The Backup Inertial Measuring Device is a sealed monoblock unit designed to measure angular velocities in three axes,…

Electromagnet EM-IF-20

The Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and…

Electromagnetic Unit (EMU) – Magnetic Torquer for Nanosatellites

The Electromagnetic Unit (EMU) is a magnetic torquer for nanosatellites, designed to create a dipole magnetic moment proportional…

Electromagnetic Unit (EMU) – Magnetic Torquer

The Electromagnetic Unit (EMU) is a magnetic torquer designed for spacecraft attitude control systems, creating a dipole magnetic…

Xenon Flow Controller for Low Power Plasma Thruster with 50 mm Diameter of the Accelerating Channel

A Xenon Flow Controller designed to provide and distribute propellant flow to low-power stationary plasma thrusters with a…

Xenon Flow Controller for Low Power Plasma Thruster with 70 mm Diameter of the Accelerating Channel

A Xenon Flow Controller designed for low-power plasma thrusters, regulating propellant flow rate and distributing it between anode…

Xenon Flow Controller for Stationary Plasma Thruster with a Discharge Power of up to 5 kW

The Xenon Flow Controller provides and distributes the required xenon propellant flow rate to Stationary Plasma Thrusters with…

Xenon Flow Controller for Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W

A Xenon Flow Controller designed for Stationary Plasma Thrusters with a nominal discharge power of 1350 W, it…

XFC unit

The XFC unit is a xenon flow controller designed to supply and regulate the total flow rate and…

Altitude Control System

An Altitude Control System (ACS) designed for spacecraft, providing orientation accuracy of 1 degree and stabilization accuracy of…

Thermocatalytic Low Thruster

A hydrazine thermocatalytic low-thrust engine used for spacecraft orientation, attitude control, and station keeping.

Thermocatalytic Thrusters

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

Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XF

A Thrust Module (TM) for spacecraft station keeping, featuring a 70 mm diameter thruster and a Xenon Flow…

TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster

The TU1 Thruster Unit is a thermocatalytic low thruster designed for spacecraft orientation and attitude control, using hydrazine…

TU3 Truster Unit Based on Modified Thermocatalytic Low Thrusters

The TU3 Truster Unit is a propulsion system designed for spacecraft orientation and attitude control, utilizing three modified…

Xenon Cold Gas Thruster

The Xenon Cold Gas Thruster is a propulsion system designed for spacecraft orientation, utilizing xenon or nitrogen propellant.…