[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.)

Keywords:Hall effect thruster, Electric propulsion, Alternative propellant, Water propellant, Small satellite