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Variable operation of Hall thruster with multiple segmented electrodes

J. Appl. Phys. 89, 2040 (2001); doi:10.1063/1.1337919

Issue Date: 15 February 2001

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N. J. Fisch, Y. Raitses, L. A. Dorf, and A. A. Litvak
Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey 08540
Variable plasma jet velocity with low beam divergence over a range of mass flow rates can be achieved through segmented electrode operation of the Hall plasma accelerator. With the use of just a cathode side electrode at the cathode potential, the beam divergence can be decreased substantially, at some cost in efficiency. However, the additional use of an anode side electrode retains the same reduced plume divergence, but at efficiencies comparable to the nonsegmented operation. The high efficiency persists also when the anode side electrode is biased at an intermediate potential, thus producing two-stage Hall accelerator operation. ©2001 American Institute of Physics.
History: Received 20 January 2000; accepted 10 November 2000
Permalink: http://link.aip.org/link/?JAPIAU/89/2040/1
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KEYWORDS and PACS

Keywords
PACS
  • 52.50.Dg
    Physics of plasmas and electric discharges Plasma production and heating Plasma sources
  • 52.75.Di
    Physics of plasmas and electric discharges Plasma devices Ion and plasma propulsion
  • YEAR: 2001

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PUBLICATION DATA

ISSN:
0021-8979 (print)   1089-7550 (online)
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