D-100-II

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D-100-II

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.

AKA: D-100. Status: Development. Thrust: 0.0650 N (0.0140 lbf). Specific impulse: 1,600 s.

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.

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

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