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Raitses, Yevgeny; Smirnov, Artem; Granstedt, Erik; Fisch, Nathaniel J.
Princeton Plasma Physics Lab., Princeton, NJ (United States). Funding organisation: USDOE Office of Science (United States)2007
Princeton Plasma Physics Lab., Princeton, NJ (United States). Funding organisation: USDOE Office of Science (United States)2007
AbstractAbstract
[en] The cylindrical Hall thruster features high ionization efficiency, quiet operation, and ion acceleration in a large volume-to-surface ratio channel with performance comparable with the state-of-the-art annular Hall thrusters. These characteristics were demonstrated in low and medium power ranges. Optimization of miniaturized cylindrical thrusters led to performance improvements in the 50-200W input power range, including plume narrowing, increased thruster efficiency, reliable discharge initiation, and stable operation.
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27 Nov 2007; 14 p; 43. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit; Cincinnati, OH (United States); 8-11 Jul 2007; ACO2-76CHO3073; Also available from OSTI as DE00961570; PURL: https://www.osti.gov/servlets/purl/961570-AQuHA1/; Propulsion and Power
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