Experimental investigation of an external discharge very low anode power (< 20 W) hall thruster
Journal of Electric Propulsion(2022)
摘要
sub 20 W wall-less Hall Effect Thruster (HET) was developed at the Asher Space Research Institute (ASRI), Technion. In this work, an initial study of the thruster performance and underlying physics was conducted. It was found that the anode efficiency of the thruster was low ( 1
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关键词
Hall thruster, Low power, Plume, Retarding potential analyzer, Plasma diagnostics
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