Effect of Magnetic Field Characteristics on Thrust Efficiency and Internal Efficiency of a Hall Thruster

Author:

Yuge Seiro,Shirasaki Atsushi,Tahara Hirokazu

Publisher

Japan Society for Aeronautical and Space Sciences

Reference16 articles.

1. 1) Milligan, D., Gestal, D., Camino, O., Estublier, D. and Koppel, C.: SMART-1 Electric Propulsion Operations, AIAA Paper 2004-3436, 2004.

2. 2) Jacobson, D. T., Manzella, D. H., Hofer, R. R. and Peterson, P. Y.: NASA’s 2004 Hall Thruster Program, AIAA Paper 2004-3600, 2004.

3. 3) Murashko, V., Koryakin, A., Nyatin, A., Kim, V., Popov, G., Romashko, A., Yermoshkin, Y., Petrusevich, V., Gorshkov, O., Koroteyev, A., Garkusha, V., Semenkin, A. and Tverdokhlebov, S.: State of the Art and Prospects of Electric Propulsion in Russia, IEPC Paper 2003-340, 2003.

4. 4) Morozov, A. I., Esipchuk, Yu. V., Kapulkin, A. M., Nevrovskii, V. A. and Smirnov, V. A.: Effect of the Magnetic Field on a Closed-Electron-Drift Accelerator, Sov. Phys. Tech. Phys., 17 (1972), pp. 482–487.

5. 5) Bishaev, A. M. and Kim, V.: Local Plasma Properties in a Hall-Current Accelerator with an Extended Acceleration Zone, Sov. Phys. Tech. Phys., 23 (1978), pp. 1055–1057.

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