[b-7] Water Propellant for Hall Thruster

[2023-b-25] Effect of channel diameter and width on a low-power water-vapor Hall thruster

*Masayuki Matsuura¹, Kento Shirasu², Hiroyuki Koizumi¹, Yuichi Nakagawa³, Hiroki Watanabe³, Hokuto Sekine², Kimiya Komurasaki² (1. Department of Advanced Energy, The University of Tokyo, 2. Department of Aeronautics and Astronautics, The University of Tokyo, 3. Pale Blue Inc.)

キーワード：Hall effect thruster, Electric propulsion, Alternative propellant, Water propellant, Small satellite