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Hall Thrusters 389 [60] D. Manzella, J. Yim, and I. Boyd, “Predicting Hall Thruster Operational Lifetime,” AIAA-2004-3953, 40th Joint Propulsion Conference, Ft. Lauderdale, Florida, July 11–14, 2004. [61] C. Boniface, L. Garrigues, G. J. M. Hagelaar, and J. P. Boeuf, “Anomalous Cross Field Electron Transport in a Hall Effect Thruster,” Applied Physics Letters, 161503, vol. 89, 2006. [62] E. Y. Choueiri, “Plasma Oscillations in Hall Thrusters,” Phys. of Plasmas, vol. 8, no. 4, pp. 1411–1426, 2001. [63] A. Ducrocq, J. C. Adam, A. Heron, and G. Laval, “High-Frequency Electron Drift Instability in the Cross-field Configuration of Hall Thrusters,” Physics of Plasmas, 102111, vol. 13, 2006. [64] V. Abgaryan, H. Kaufman, V. Kim, D. Ovsyanko, I. Shkarban, A. Semenov, A. Sorokin, and V. Zhurin, “Calculation Analysis of the Erosion of the Discharge Chamber Walls and Their Contamination During Prolonged SPT Operation,” AIAA-94-2859, 30th Joint Propulsion Conference, Indianapolis, Indiana, June 27–29, 1994. [65] Y. Garnier, V. Viel, J. F. Roussel, and J. Bernard, “Low Energy Xenon Ion Sputtering of Ceramics Investigated for Stationary plasma Thrusters,” Journal of Vacuum Science Technology A, vol. 17, pp. 3246–3254, 1999. [66] Y. Yamamura and H. Tawara, “Energy Dependence of Ion-Induced Sputtering from Monatomic Solids at Normal Incidence,” Atomic Data and Nuclear Data Tables, vol. 62, pp. 149–253, 1996. [67] S. K. Absalamov, V. Andrew, T. Colberi, M. Day, V. V. Egorov, R. U. Gnizdor, H. Kaufman, V. Kim, A. I. Korakin, K. N. Kozubsky, S. S. Kudravzev, U. V. Lebedev, G. A. Popov, and V. V. Zhurin, “Measurement of Plasma Parameters in the Stationary Plasma Thruster (SPT-100) Plume and its Effect on Spacecraft Components,” AIAA-1992- 3156, 28th Joint Propulsion Conference, Nashville, Tennessee, July 6–8, 1992. Homework Problems 1. You want to design an experimental Hall thruster to operate from 100 to 800 V and from 100 to 300 gauss. Assuming that the electron temperature is always about 10% of the discharge voltage, what are the minimum and maximum lengths of the magnetized region in the channel to have a factor of 5 margin against electron and ion orbit limits? Neglect collisions. 2. Derive Eq. (7.3-42).PDF Image | Fundamentals of Electric Propulsion: Ion and Hall Thrusters
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