ISTS2023

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Oral Session

b) Electric and Advanced Propulsion

[b-9] Alternative Propellant for Hall Thruster

Thu. Jun 8, 2023 2:00 PM - 3:00 PM Kurumeza 3F (Kurumeza 3F)

Hirokazu Tahara (Osaka Sangyo University),Keita Nishii (Tokyo Metropolitan University)

2:00 PM - 2:20 PM

[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)

Keywords:Hall thruster, Neutral particle velocity, Anode temperature