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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 .
