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Flight Ion and Hall Thrusters 443 and JPL have jointly investigated the applicability of the BPT-4000 to NASA deep-space missions [43] where throttle range and efficiency are important. The throttleability of the BPT-4000 engine [44] from power levels 1 kW to 4.5 kW was demonstrated with very high efficiency observed at low power levels for this size thruster. Hall thruster technology will continue to be developed and used in commercial and scientific missions due to their high performance and relatively simple construction and operation. References [1] S. Shimada, K. Satho, Y. Gotoh, E. Nistida, I. Terukina, T. Noro, H. Takegahara, K. Nakamaru, and H. Nagano, “Development of an Ion Engine System for ETS-6,” IEPC-93-009, 23rd International Electric Propulsion Conference, Seattle, Washington, September 1993. [2] T. Ozaki, E. Nishida, and Y. Gotoh, “Development Status of 20mN Xenon Ion Thruster,” AIAA-2000-3277, 36th Joint Propulsion Conference, Huntsville, Alabama, July 16–19, 2000. [3] J. R. Beattie, “XIPS Keeps Satellites on Track,” The Industrial Physicist, June 1998. [4] J. R. Beattie, J. D. Williams, and R. R. Robson, “Flight Qualification of an 18-mN Xenon Ion Thruster,” IEPC 93-1015, 23rd International Electric Propulsion Conference, Seattle, Washington, September 1993. [5] M. J. Patterson, T. W. Haag, V. K. Rawlin, and M. T. Kussmaul, “NASA 30-cm Ion Thruster Development Status,” AIAA-1994-2849, 30th Joint Propulsion Conference, Indianapolis, Indiana, June 27–29, 1994. [6] J. R. Brophy, “NASA’s Deep Space 1 Ion Engine,” Review of Scientific Instruments, vol. 73, pp. 1071–1078, 2002. [7] J. R. Brophy, M. Marcucci, G. Ganapathi, C. Garner, M. Henry, B. Nakazono, and D. Noon, “The Ion Propulsion System for Dawn,” AIAA 2003-4542, 39th Joint Propulsion Conference, Huntsville, Alabama, July 20–23, 2003. [8] http://www.l-3com.com/eti/product_lines_electric_propulsion.htm [9] J. R. Beattie, J. N. Matossian, and R. R. Robson, “Status of Xenon Ion Propulsion Technology,” Journal of Propulsion and Power, vol. 6, pp. 145–150, 1990. [10] D. M. Goebel, M. Martinez-Lavin, T. A. Bond, and A. M. King, “Performance of XIPS Electric Propulsion in Station Keeping of the Boeing 702 Spacecraft,” AIAA-2002-5117, 38th Joint Propulsion Conference, Indianapolis, Indiana, July 7–10, 2002.PDF Image | Fundamentals of Electric Propulsion: Ion and Hall Thrusters
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