This page no longer updated from 31 October 2001. Latest version can be found at Hall Electric Thruster

Hall -

Credit: Boeing / Rocketdyne. 5,748 bytes. 127 x 156 pixels.

Designer: Rocketdyne. Developed in: 1999. Propellants: Electric/Xenon Thrust(vac): 0 kgf. Isp: 3,500 sec. Comments: 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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Last update 12 March 2001.
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© Mark Wade, 2001 .