Encyclopedia Astronautica

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
  • TsNIIMASH Russian manufacturer of rocket engines. Central Scientific-Research Institute for Machine Building, Russia. More...

Associated Propellants
  • 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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