Multichannel hall effect thruster

Electric lamp and discharge devices: systems – High energy particle accelerator tube – Magnetic field acceleration means

Reexamination Certificate

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Details

C315S506000, C315S111610, C244S158100, C250S42300F

Reexamination Certificate

active

07030576

ABSTRACT:
A Hall effect thruster for propelling spacecraft and satellites includes at least two acceleration channels, each of the channels has a closed end and an open end, and a plurality of flux guides adjacent each of the channels. The plurality of flux guides includes an innermost flux guide, an outermost flux guide, and at least one intermediate flux guide. Each intermediate flux guide helps provide a magnetic field to each of two adjacent acceleration channels.

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patent: 5847493 (1998-12-01), Yashnov et al.
patent: 6158209 (2000-12-01), Latischev et al.
patent: 6215124 (2001-04-01), King
patent: 6279314 (2001-08-01), Valentian et al.

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