TM-50

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TM-50

Part of TAL

TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer, designed for satellite orbital raising. Taken to engineering model stage.

Status: Development. Thrust: 0.25 N (0.05 lbf). Specific impulse: 3,000 s.

Thrust 100 to 250 mN, power requirement 20 to 50 kW, specific impulse 3000-7000 seconds, efficiency 75%.

Electrical Input Power: 50.00 kW.

Country: Russia. Propellants: Electric/Xenon. Agency: TsNIIMash.

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