[b-9] Alternative Propellant for Hall Thruster

[2023-b-32] Performance of Anode Layer thruster RAIJIN66 with Argon Propellant based on Anode Temperature Change

*Dibyesh Satpathy¹, Hokuto Sekine¹, Rei Kawashima², Kimiya Komurasaki¹, Hiroyuki Koizumi¹ (1. The University of Tokyo, 2. Shibaura Institute of Technology)

キーワード：Hall thruster, Neutral particle velocity, Anode temperature