[B-3] Hall Thrusters 2

[2022-b-15] New Discharge Power Supply of 6-kW Hall Thruster using Voltage-Doubler-Type Rectifier

*Yoshiki Matsunaga¹, Hiroki Watanabe¹, Shun Imai¹, Hiroaki Kusawake¹, Toru Takahashi², Kazuhiro Kajiwara³, Fujio Kurokawa³, Ikkoh Funaki¹ (1. Japan Aerospace Exploration Agency, 2. Takahashi Denki Seisakusho Corporation, 3. Nagasaki Institute of Applied Science)

Keywords:Hall thruster, PPU, Digital control, Voltage doubler rectifier