1. 1) Funaki, I., Cho, S., Sano, T., Fukatsu, T., Tashiro, Y., Shiiki, T., and Nakamura, Y.: Status Report on the Development of a Hall Thruster for Japanese All-Electric Propulsion Satellite, The Japan Society for Aeronautical and Space Sciences, 66 (2018), pp. 346-351 (in Japanese).
2. 2) Choueiri, E. Y.: Plasma Oscillations in Hall Thrusters, Physics of Plasmas, 8 (2001), pp. 1411-1426.
3. 3) Fukushima, Y., Yokota, S., Komurasaki, K., and Arakawa, Y.: Discharge Stabilization for an Anode-Layer-Type Hall Thruster by Azimuthally Nonuniform Propellant Supply, The Japan Society for Aeronautical and Space Sciences, 58 (2010), pp. 8-14 (in Japanese).
4. 4) Bugrova, A. I., Morozov, A. I., and Kharchevnikov, V. K.: Experimental Investigation of Near Wall Conductivity, Sov. Phys. Tech. Phys., 16 (1990), pp. 849-856.
5. 5) Kawashima, R., Hara, K., and Komurasaki, K.: Numerical Analysis of Azimuthal Rotating Spokes in a Crossed-field Discharge Plasma, Plasma Sources Science and Technology, 27 (2018), 035010.