[p-1] b) Electric and Advanced Propulsion

[2023-b-79] Discharge characteristics of 100 W-class Hall thruster with a thoriated tungsten filament cathode for a 2U CubeSat

*Seongsu Kim¹, Youngho Kim², Jaehong Park², Jaejun Lee¹, Dongha Park³, Wonho Choe³ (1. Korea Advanced Institute of Science and Technology, Department of Aerospace Engineering, Space Exploration Engineering Program, 2. Korea Advanced Institute of Science and Technology, Department of Nuclear and Quantum Engineering, Space Exploration Engineering Program, 3. Korea Advanced Institute of Science and Technology, Department of Nuclear and Quantum Engineering)

Keywords:Electric Propulsion, Hall thruster, Thoriated Tungsten Filament, CubeSat