TAL-WSF

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TAL-WSF

Part of TAL

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

TsNIIMash electric/xenon rocket engine. Hall effect thruster with anode layer. Export version of D-55 thruster developed under NASA/BMDO contract for flight test under RHETT-II program. Used for WSF satellite orbital altitude maintenance.

AKA: D-55. Status: Development. Thrust: 0.0120 N (0.0020 lbf). Specific impulse: 1,350 s.

Taken to flight model stage. Thrust 4 to 12 mN, power requirement 0.8 to 2.5 kW, specific impulse 1350-2750 seconds, efficiency 55%.

Electrical Input Power: 2.50 kW.

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

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