Improving the Hall Thruster Global Efficiency over a Wide Flow-Rate Range

Fan, HT; Li, H; Mao, W; Ding, YJ; Wei, LQ; Yu, DR

Fan, HT (corresponding author), Harbin Inst Technol, Lab Plasma Propuls, Harbin 150001, Peoples R China.; Fan, HT (corresponding author), Harbin Inst Technol, Minist Ind & Informat Technol, Key Lab Aerosp Plasma Prop, Harbin 150001, Peoples R China.

JOURNAL OF PROPULSION AND POWER, 2021; 37 (4): 625

Abstract

In this study, a 1.35 kW HEP-100X Hall thruster is used to explore effective methods for improving the global efficiency of a Hall thruster across a w......

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