Electromagnet EM-IF-20
GlavkosmosThe Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and…
6213 satellite platforms, components and ground equipment from manufacturers worldwide.
The Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and…
The Electromagnetic Unit (EMU) is a magnetic torquer for nanosatellites, designed to create a dipole magnetic moment proportional…
The Electromagnetic Unit (EMU) is a magnetic torquer designed for spacecraft attitude control systems, creating a dipole magnetic…
A Xenon Flow Controller designed to provide and distribute propellant flow to low-power stationary plasma thrusters with a…
A Xenon Flow Controller designed for low-power plasma thrusters, regulating propellant flow rate and distributing it between anode…
The Xenon Flow Controller provides and distributes the required xenon propellant flow rate to Stationary Plasma Thrusters with…
A Xenon Flow Controller designed for Stationary Plasma Thrusters with a nominal discharge power of 1350 W, it…
The XFC unit is a xenon flow controller designed to supply and regulate the total flow rate and…
An Altitude Control System (ACS) designed for spacecraft, providing orientation accuracy of 1 degree and stabilization accuracy of…
A hydrazine thermocatalytic low-thrust engine used for spacecraft orientation, attitude control, and station keeping.
Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…
A Thrust Module (TM) for spacecraft station keeping, featuring a 70 mm diameter thruster and a Xenon Flow…
The TU1 Thruster Unit is a thermocatalytic low thruster designed for spacecraft orientation and attitude control, using hydrazine…
The TU3 Truster Unit is a propulsion system designed for spacecraft orientation and attitude control, utilizing three modified…
The Xenon Cold Gas Thruster is a propulsion system designed for spacecraft orientation, utilizing xenon or nitrogen propellant.…
The Propulsion System (PS) for Nanosatellite Platform is an electrothermal propulsion unit designed for orbital maneuvering of cubesat-class…
A thermocatalytic thruster unit designed for spacecraft station keeping, utilizing hydrazine propellant and featuring redundant components for reliability.
A thermocatalytic thruster unit designed for spacecraft station keeping, utilizing hydrazine propellant and featuring main and redundant thrusters,…
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