483 satellite platforms, components and ground equipment from manufacturers worldwide.
The RD-171 M is a powerful liquid rocket engine designed for the first stage of the Zenit launch…
The RD-180 is a liquid rocket engine with afterburning of oxidizing gas, designed for the first stage of…
The RD-181 is a liquid rocket engine with afterburning of oxidizing gas, designed for the first stage of…
The RD-182 (120M) is a liquid-propellant rocket engine, a terrestrial modification of the RD120MS, designed for the first…
The Pressure Sensor Vt 212 is a strain gauge sensor designed for measuring static-dynamic pressure in liquid and…
RD-120MS is a modification of the RD-120 liquid rocket engine with afterburning of oxidizing gas, intended for the…
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…
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…
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