Hall Electric Thruster

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Hall
Credit - Boeing / Rocketdyne

Engine Model: Hall Electric Thruster. Designer: Rocketdyne. Developed in: 1999. Propellants: Electric/Xenon. Thrust(vac): 3.00 N (0.60 lbf). Throttled thrust(vac): 0.80 N (0.17 lbf). Isp: 1,600 sec. Country: Russia. Status: Development.

TsNIIMASH (Russia)/Rocketdyne, Satellite Thruster. Electric, pressure-fed. Variable 80 mN - 3.0 N thrust, specific impulse 1600 to 3500 seconds. Satellite orbit raising and station-keeping applications.

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