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Ion Thruster Plasma Generators 185 [42] J. M. Lafferty, Foundations of Vacuum Science and Technology, New York: John Wiley and Sons, 1998. [43] Y. Hayakawa, K. Miyazaki, and S. Kitamura, “Measurements of Electron Energy Distributions in a 14-cm Diameter Ring Cusp Ion Thruster,” Journal of Propulsion and Power, vol. 8, pp. 118–126, 1992. [44] D. Herman, “Discharge Cathode Electron Energy Distribution Functions in a 40-cm NEXT-type Ion Engine,” AIAA-2005-4252, 41st AIAA Joint Propulsion Conference, Tucson, Arizona, July 10–13, 2005. [45] D. Bohm, Chapter 1, The Characteristics of Electric Discharges in Magnetic Fields, edited by A. Guthrie and R. Wakerling, New York: McGraw-Hill, pp. 1–76, 1949. [46] N. L. Milder, “A Survey and Evaluation of Research on the Discharge Chamber Plasma of a Kaufman Thruster,” AIAA-69-494, 5th Propulsion Joint Specialist Conference, U.S. Air Force Academy, Colorado Springs, Colorado, June 9–13, 1969. [47] H. R. Kaufman, “Performance of Large Inert-Gas Thrusters,” AIAA- 81-0720, 15th International Electric Propulsion Conference, Las Vegas, Nevada, April 21–23, 1981. [48]T. Ozaki, E. Nishida, Y. Gotoh, A. Tsujihata, and K. Kajiwara, “Development Status of a 20 mN Xenon Ion Thruster,” AIAA-2000-3277, 36th Joint Propulsion Conference, Huntsville, Alabama, July 16–19, 2000. [49] W. F. Divergilio, H. Goede, and V. V. Fosnight, “High Frequency Plasma Generators for Ion Thrusters,” NASA #CR-167957, November 1981. [50] H. J. Leiter, R. Killinger, H. Bassner, J. Miller, R. Kulies, and T. Fröhlich, “Evaluation of the Performance of the Advanced 200 mN Radio Frequency Ion Thruster RIT_XT,” AIAA-2002-3836, 38th Joint Propulsion Conference, Indianapolis, Indiana, July 7–10, 2002. [51]M. Tuszewski, “Inductive Electron Heating Revisited,” Physics of Plasmas, vol. 4, pp. 1922–1928, 1997. [52] H. Goede, “30-cm Electron Cyclotron Plasma Generator,” Journal of Spacecraft, vol. 24, no. 5, p. 437, 1987. [53] H. Kuninaka and S. Satori, “Development and Demonstration of a Cathode-less Electron Cyclotron Resonance Ion Thruster,” Journal of Propulsion and Power, vol. 14, pp. 1022–1026, 1998. [54] H. Kuninaka, I. Funaki, and K. Toki, “Life Test of Microwave Discharge Ion Thrusters for MUSES-C in Engineering Model Phase,” AIAA-99- 2439, 35th Joint Propulsion Conference, Los Angeles, California, June 20– 24, 1999.PDF Image | Fundamentals of Electric Propulsion: Ion and Hall Thrusters
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