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Mathematical Problems in Engineering
Volume 2015 (2015), Article ID 418493, 8 pages
http://dx.doi.org/10.1155/2015/418493
Research Article

Numerical Simulation of Interaction between Hall Thruster CEX Ions and SMART-1 Spacecraft

1Department of Mechanical Engineering and Automation, Harbin Institute of Technology Shenzhen Graduate School, Shenzhen, Guangdong 518055, China
2Department of Natural Sciences and Humanities (Mathematics/Mechanics/Humanities), Harbin Institute of Technology Shenzhen Graduate School, Shenzhen, Guangdong 518055, China

Received 11 June 2014; Accepted 13 September 2014

Academic Editor: Junuthula N. Reddy

Copyright © 2015 Kang Shan et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. I. D. Boyd and J. P. W. Stark, “Modeling of a small hydrazine thruster plume in the transition flow regime,” Journal of Propulsion and Power, vol. 6, no. 2, pp. 121–126, 1990. View at Publisher · View at Google Scholar · View at Scopus
  2. J. H. Park, S. W. Back, and J. S. Kim, “Direct simulation Monte Carlo analysis of thruster plumes/satellite base region interaction,” AIAA Journal, vol. 42, no. 8, pp. 1622–1632, 2004. View at Publisher · View at Google Scholar · View at Scopus
  3. I. D. Boyd and A. Ketsdever, “Interactions between spacecraft and thruster plumes,” Journal of Spacecraft and Rockets, vol. 38, no. 3, p. 380, 2001. View at Publisher · View at Google Scholar · View at Scopus
  4. F. E. Lumpkin III, J. Marichalar, and B. D. Stewart, “High fidelity simulations of plume impingement to the international space station,” in Proceedings of the 33rd JANNAF Exhaust Plume and Signatures Subcommittee Meeting, Monterey, Calif, USA, December 2012.
  5. Z.-J. Xiao, H.-E. Cheng, and H.-L. Zhou, “Plume interaction in parallel multi-thrusters propulsion system and the effect on backflow,” in Proceedings of the 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, pp. 1963–1972, San Francisco, Calif, USA, June 2006. View at Scopus
  6. G. Markelov and E. Gengembre, “Modeling of plasma flow around SMART-1 spacecraft,” IEEE Transactions on Plasma Science, vol. 34, no. 5, pp. 2166–2175, 2006. View at Publisher · View at Google Scholar · View at Scopus
  7. I. D. Boyd and J. T. Yim, “Modeling of the near field plume of a Hall thruster,” Journal of Applied Physics, vol. 95, no. 9, pp. 4575–4584, 2004. View at Publisher · View at Google Scholar · View at Scopus
  8. A. Passaro, A. Vicini, F. Nania, and L. Biagioni, “Numerical rebuilding of smart-1 plasma plumespacecraft interaction,” IEPC Paper IEPC-2005-174, 2005. View at Google Scholar
  9. V. A. S. Y. A. Bondar, “Modeling of plume of stationary plasma thruster by particle method,” Thermophysics and Aeromechanics, vol. 38, no. 3, pp. 373–392, 2001. View at Google Scholar
  10. L. Yan, P.-Y. Wang, Y.-H. Ou, and X.-L. Kang, “Numerical study of hall thruster plume and sputtering erosion,” Journal of Applied Mathematics, vol. 2012, Article ID 327021, 16 pages, 2012. View at Publisher · View at Google Scholar · View at Scopus
  11. R. Kafafy and Y. Cao, “Modelling ion propulsion plume interactions with spacecraft in formation flight,” Aeronautical Journal, vol. 114, no. 1157, pp. 417–426, 2010. View at Google Scholar · View at Scopus
  12. M. Tajmar, J. González, and A. Hilgers, “Modeling of spacecraft-environment interactions on SMART-1,” Journal of Spacecraft and Rockets, vol. 38, no. 3, pp. 393–399, 2001. View at Publisher · View at Google Scholar · View at Scopus
  13. I. D. Boyd, “Numerical simulation of hall thruster plasma plumes in space,” IEEE Transactions on Plasma Science, vol. 34, no. 5, pp. 2140–2147, 2006. View at Publisher · View at Google Scholar · View at Scopus
  14. G. A. Bird, Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford University Press, Oxford, UK, 1994. View at MathSciNet
  15. R. Kafafy, T. Lin, Y. Lin, and J. Wang, “Three-dimensional immersed finite element methods for electric field simulation in composite materials,” International Journal for Numerical Methods in Engineering, vol. 64, no. 7, pp. 940–972, 2005. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  16. J. Wang, Y. Cao, R. Kafafy, J. Pierru, and V. K. Decyk, “Simulations of ion thruster plume-spacecraft interactions on parallel supercomputer,” IEEE Transactions on Plasma Science, vol. 34, no. 5, pp. 2148–2158, 2006. View at Publisher · View at Google Scholar · View at Scopus
  17. M. Tajmar, R. Sedmik, and C. Scharlemann, “Numerical simulation of SMART-1 Hall-thruster plasma interactions,” Journal of Propulsion and Power, vol. 25, no. 6, pp. 1178–1188, 2009. View at Publisher · View at Google Scholar · View at Scopus
  18. C. K. Birdsall, “Particle-in-cell charged-particle simulations, plus Monte Carlo collisions with neutral atoms, PIC-MCC,” IEEE Transactions on Plasma Science, vol. 19, no. 2, pp. 65–85, 1991. View at Publisher · View at Google Scholar · View at Scopus
  19. S. Pullins, R. Dressler, Y. Chiu, and D. Levandier, “Thrusters: Xe++Xe symmetric charge transfer,” in Proceedings of the 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nev, USA, January 2000.
  20. J. S. Miller, S. H. Pullins, D. J. Levandier, Y.-H. Chiu, and R. A. Dressler, “Xenon charge exchange cross sections for electrostatic thruster models,” Journal of Applied Physics, vol. 91, no. 3, pp. 984–991, 2002. View at Publisher · View at Google Scholar · View at Scopus