Hall Electric Thruster

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Hall Electric Thruster

Part of TAL

Hall
Credit: Boeing / Rocketdyne

TsNIIMash / Rocketdyne electric/xenon rocket engine. Development. Satellite orbit raising and station-keeping applications. Electric, pressure-fed. Variable 80 mN - 3.0 N thrust, specific impulse 1600 to 3500 seconds.

Status: Development. Date: 1999. Thrust: 3.00 N (0.60 lbf). Specific impulse: 1,600 s.

Throttled thrust(vac): 0.80 N (0.17 lbf).

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

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