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Segmented electrode hall thruster with reduced plume

United States Patent

August 17, 2004
View the Complete Patent at the US Patent & Trademark Office
Princeton Plasma Physics Laboratory - Visit the Office of Technology Transfer Website
An apparatus and method for thrusting plasma, utilizing a Hall thruster with segmented electrodes along the channel, which make the acceleration region as localized as possible. Also disclosed are methods of arranging the electrodes so as to minimize erosion and arcing. Also disclosed are methods of arranging the electrodes so as to produce a substantial reduction in plume divergence. The use of electrodes made of emissive material will reduce the radial potential drop within the channel, further decreasing the plume divergence. Also disclosed is a method of arranging and powering these electrodes so as to provide variable mode operation.
Fisch; Nathaniel J. (Princeton, NJ), Raitses; Yevgeny (Princeton, NJ)
General Plasma Technologies LLC (Princeton, NJ)
09/ 834,373
April 13, 2001
CONTRACTUAL ORIGIN OF THE INVENTION AND STATEMENT AS TO FEDERALLY SPONSORED RESEARCH Pursuant to 35 U.S.C. 202(c), it is acknowledged that the U.S. Government has certain rights in the invention described herein which was made in part with funds from the Department of Energy under Grant No. DE-AC02-76-CHO-3073 under contract between the U.S. Department of Energy and Princeton University. Princeton University has served notice that it does not wish to retain title to this invention.