541 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with…
In terms of discharge power it has been forced up to 1250 W. Propellant - xenon. Consists of…
Thruster with a discharge power of up to 5 kW. Propellant - xenon. Consists of the anode and…
Flight-proven low-power Hall thruster (18 mN, 350 W, Isp 1450 s, 2 kg) for small spacecraft ≤500 kg;…
High-power sustainer Hall thruster (520 mN, 10.5 kW, Isp 2580 s, 11.8 kg) for spacecraft transportation missions.
Multimode Hall thruster (200/380 mN, 3.5/6 kW, Isp 1700/2650 s, 8 kg) for 3000 kg spacecraft, qualification model.
Integrated Thruster Unit (ITU) includes a high-precision thruster orientation mechanism (TOM) and two propulsion systems based on the…
ITU-5000M includes a high-precision Thruster Orientation Mechanism (TOM) and a propulsion system based on the Modified Stationary Plasma…
Electric propulsion. It has high specific impulse at relatively low power. The record number of burnings is up…
Hall-effect electric thruster (95 mN, <2.4 kW, Isp 2680 s, 5.25 kg) for 2500–3000 kg spacecraft, record specific…
Flight-proven multimode Hall thruster (80/115 mN, 1.35/2.0 kW, Isp >1550 s, 5.2 kg) flown on Express-A4 (2002).
High specific impulse Hall thruster (72 mN, 1.65 kW, Isp 2680 s, 6 kg) for 3000 kg spacecraft;…
Flight-proven ammonia CPS for orbit/attitude correction and flywheel momentum dump (5000–5500 N·s total impulse, 0.02–0.8 N thrust, ≤17…
Flight-proven cold-gas thruster (0.73–0.82 N He/N2, 0.105 kg, 80,000 starts) for precise spacecraft attitude control, flown on KOSMOS…
Consists of two units: Stationary Plasma Thruster with a nominal discharge power of 1350 W and Xenon Flow…
Corrective propulsion system (CPS) consists of a monoblock, including an AIPD-95 CPS engine, a BPU-150 device, a set…
The corrective propulsion system of the UD-AIPD consists of a monoblock, including the KNE block, the BIR1, BIR2…
Dual operating mode: 1.35 / 2.5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical…
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