TAL-38

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TAL-38

Part of TAL

TAL-38
TAL-38 HAL effect thruster
Credit: TsNIIMASH

TsNIIMash electric/xenon rocket engine. Development. Hall effect thruster with anode layer. Export version of D-38, developed under NASA contract for satellite station-keeping and attitude control. Taken to engineering model stage.

AKA: D-38. Status: Development. Thrust: 0.0080 N (0.0017 lbf). Specific impulse: 2,500 s.

Thrust 2.5 to 8 mN, power requirement 0.4 to 1.0 kW, specific impulse 1300-2500 seconds, efficiency 45%.

Electrical Input Power: 1.00 kW.

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

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