Fundamentals of Electric Propulsion: Ion and Hall Thrusters

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Fundamentals of Electric Propulsion: Ion and Hall Thrusters ( fundamentals-electric-propulsion-ion-and-hall-thrusters )

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Ion Thruster Plasma Generators 183 [14] J. R. Beattie, J. N. Matossian, and R. R. Robson, “Status of Xenon Ion Propulsion Technology,” Journal of Propulsion and Power, vol. 7, pp. 145–150, 1990. [15] T. D. Maske, “Plasma Properties and Performance of Mercury Ion Thrusters,” AIAA Journal, vol. 9, pp. 205–212, 1971. [16] J. Ward and T. Masek, “A Discharge Computer Model for an Electron Bombardment Thruster,” AIAA-1976-1009, AIAA International Electric Propulsion Conference, Key Biscayne, Florida, November 14–17, 1976. [17] J. N. Matossian and J. R. Beattie, “Model for Computing Volume Averaged Plasma Properties in Electron-Bombardment Ion Thrusters,” Journal of Propulsion and Power, vol. 5, pp.188–196, 1989. [18] J. R. Brophy, Ion Thruster Performance Model, NASA CR-174810, Ph.D. Thesis, Colorado State University, Fort Collins, Colorado, December 1984. [19] J. R. Brophy and P. J. Wilbur, “Simple Performance Model for Ring and Line Cusp Ion Thrusters,” AIAA Journal, vol. 23, no. 11, pp. 1731–1736, 1985. [20] D. M. Goebel, J. E. Polk, and A. Sengupta, “Discharge Chamber Performance of the NEXIS Ion Thruster,” AIAA-2004-3813, 40th AIAA Joint Propulsion Conference, Fort Lauderdale, Florida, July 11–14, 2004. [21] D. M. Goebel, R. E. Wirz, and I. Katz, “Analytical Ion Thruster Discharge Performance Model,” AIAA-2006-4486, 42nd Joint Propulsion Conference, Sacramento, California, July 10–13, 2006. [22] D. M. Goebel, “Ion Source Discharge Performance and Stability,” Physics of Fluids, vol. 25, no. 6, pp. 1093–1102, 1982. [23] A. T. Forrester, Large Ion Beams, New York: John Wiley and Sons, 1988. [24] M. Lieberman and A. Lichtenberg, Principles of Plasma Discharges and Materials Processing, New York: John Wiley and Sons, 1994. [25] Maxwell 3-D is a product of Ansoft Corp., http://www.ansoft.com/products/em/max3d/overview.cfm. [26] R. E. Wirz and D. M. Goebel, “Ion Thruster Discharge Performance per Magnetic Field Geometry,” AIAA-2006-4487, 42nd Joint Propulsion Conference, Sacramento, California, July 10–13, 2006. [27] K. Leung, N. Hershkowitz, and K. MacKenzie, “Plasma Confinement by Localized Cusps,” Physics of Fluids, vol. 19, no. 7, pp. 1045–1053, 1976. [28] D. Rapp and P. Englander-Golden, “Total Cross Sections for Ionization and Attachment in Gases by Electron Impact. I. Positive Ionization,” The Journal of Chemical Physics, vol. 43, no. 5, pp. 1464–1479, 1965.

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