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Volume 34 Issue 05
May  2008
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Journal of Beijing University of Aeronautics and Astronautics  > 2008  >  34(05): 584-586.
WANG Liang, LIN Yan-zhi, WANG Zhan-linet al. Flight Director Signal Synthesis for Landing Approach Operation Based on Optimal FCZPETC[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 312-315. (in Chinese)
Citation: Yao Jie, Tang Haibin, Wang Haixing, et al. Three-dimension numerical simulation of working process of space plasma sail[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(05): 584-586. (in Chinese)
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Three-dimension numerical simulation of working process of space plasma sail

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 08 May 2007
  • Publish Date: 31 May 2008
    Abstract
  • Using three-dimension model, the hybrid particle in cell method was used to simulate the interaction between the inflated magnetic field and solar wind. The interaction between solar wind particles and dipole magnetic field produced by coil was studied after the plasma injecting into the dipole magnetic field. The changing of solar wind and magnetic field was compared when the plasma was injected with different velocity. It is shown that the bow shock like-structure caused by the interaction between solar wind and dipole magnetic field appears at the area where the magnetic pressure and the dynamic solar wind pressure balance each other. The magnetic field inflates when high-energy density plasma was injected into the dipole magnetic field, then the magnetic field expels the solar wind particles outward. The bow shock like-structure changes and it increases the cross area with the solar wind. It is shown that the bigger the velocity of injected plasma, the more clear the magnetic field inflation and the stronger the interaction with solar wind.

     

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  • [1] Winske D, Omidi N. Plasma expansion in the presence of a dipole magnetic field[J].Physics of Plasmas, 2005, 12(7):072514 [2] Winglee R M, Slough J, Ziemba T, et al. Mini-magnetospheric plasma propulsion: tapping the energy of the solar wind for spacecraft propulsion[J]. Journal of Geophysical Research, 2000, 105:21067-21077 [3] Winglee R M. Multi-fluid simulations of the magnetosphere: the identification of the geopause and its variation with IMF[J]. Geophysical Research Letters, 1998, 25:4441-4444 [4] Winglee R, Ziemba T, Giersch L, et al. Simulation of mini-magnetospheric plasma propulsion (M2P2) interacting with an external plasma wind .AIAA-2003-5224,2003 [5] Zubrin R M.The use of magnetic sails to escape from low earth orbit[J].Journel of the British Interplanetary Society, 1993, 46: 3-10 [6] Saha S. Modeling of plasma propulsion using an inflated magnetic field and its interaction with a fast plasma stream .Huntsville: Department of electrical and computer enyineering,University of Alabama, 2003 [7] Huba J D, Hassan A B, Winske D. Stability of sub-Alfvenic plasma expansions [J]. Physics of Fluids B, 1990, 2:1676-1697 [8] Winske D. Development of flute modes on expanding plasma clouds [J]. Physics of Fluids B, 1989, 1: 1900-1910
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