TsNIIMASH electric/xenon rocket engine. 65 mN. Development. Isp=1600s. Hall effect thruster with anode layer, designed for satellite orbital raising. Taken to engineering model stage.
Thrust 8 to 65 mN, power requirement 1.3 to 15 kW, specific impulse 1600-4250 seconds, efficiency 65%.
Electrical Input Power: 15.00 kW.
Status: Development.
Thrust: 0.0650 N (0.0140 lbf).
Specific impulse: 1,600 s.
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Associated Countries
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Associated Manufacturers and Agencies
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TsNIIMASH Russian manufacturer of rocket engines. Central Scientific-Research Institute for Machine Building, Russia. More...
Associated Propellants
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Electric/Xenon The many versions of electric engines use electric or magnetic fields to accelerate ionized elements to high velocity, creating thrust. The power source can be a nuclear reactor or thermal-electric generator, or solar panels. Proposed as propellant for some ion motors. More...
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