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384 Chapter 7 References [1] S. D. Grishin and L. V. Leskov, Electrical Rocket Engines of Space Vehicles, Moscow, Russia: Mashinostroyeniye Publishing House (published in Russian) , 1989. [2] H. R. Kaufman, “Technology of Closed-Drift Thrusters,” AIAA Journal, vol. 23, no. 1, pp. 78–87, 1985. [3] V. V. Zhurin, H. R. Kaufman, and R. S. Robinson, “Physics of Closed Drift Thrusters,” Plasma Sources Science and Technology, vol. 8, no. 1, pp. R1–R20, 1999. [4] V. Kim, “Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters,” Journal of Propulsion and Power, vol. 14, no. 5, pp. 736–743, 1998. [5] A. I. Morosov and V. V. Savelyev, “Fundamentals of Stationary Plasma Thruster Theory,” in Reviews of Plasma Physics, edited by B. B. Kadomtsev and V. D. Shafranov, vol. 21, New York: Kluwer Academic/Plenum Publishers, 2000. [6] J. R. Brophy, J. W. Barnett, J. M. Sankovic, and D. A. Barnhart, “Performance of the Stationary Plasma Thruster: SPT-100,” AIAA-92- 3155, 28th Joint Propulsion Conference, Nashville, Tennessee, July 6–8, 1992. [7] B. A. Arhipov, L. Z. Krochak, S. S. Kudriavcev, V. M. Murashko, and T. Randolph, “Investigation of the Stationary Plasma Thruster (SPT-100) Characteristics and Thermal Maps at the Raised Discharge Power,” AIAA-98-3791, 34th Joint Propulsion Conference, Cleveland, Ohio, July 13–15, 1998. [8] L. B. King, “A Re-examination of Electron Motion in Hall Thruster Fields,” IEPC-2005-258, 29th International Electric Propulsion Conference, Princeton University, New Jersey, October 31–November 4, 2005. [9] R. R. Hofer, R. S. Jankovsky, and A. D. Gallimore, “High-Specific Impulse Hall Thrusters, Part 1: Influence of Current Density and Magnetic Field,” Journal of Propulsion and Power, vol. 22, no. 4, pp. 721–731, 2006. [10] R. R. Hofer and A. D. Gallimore, “High-Specific Impulse Hall Thrusters, Part 2: Efficiency Analysis,” Journal of Propulsion and Power, vol. 22, no. 4, pp. 732–740, 2006. [11] R. R. Hofer, “Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters,” Ph.D. Dissertation, Aerospace Engineering, University of Michigan, Ann Arbor, Michigan, 2004.PDF Image | Fundamentals of Electric Propulsion: Ion and Hall Thrusters
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