Advanced Search+
Peng HU (胡鹏), Daren YU (于达仁), Yan SHEN (沈岩). Magnet stage optimization of 5 kW multicusped field thruster[J]. Plasma Science and Technology, 2020, 22(9): 94015-094015. DOI: 10.1088/2058-6272/aba680
Citation: Peng HU (胡鹏), Daren YU (于达仁), Yan SHEN (沈岩). Magnet stage optimization of 5 kW multicusped field thruster[J]. Plasma Science and Technology, 2020, 22(9): 94015-094015. DOI: 10.1088/2058-6272/aba680

Magnet stage optimization of 5 kW multicusped field thruster

  • The multi-cusped field thruster is a unique electric thruster device, which has many advantages such as long lifetime, large-range thrust throttling ability, high thrust density, and low mass. The thruster employs several alternating polarity permanent magnets to create a periodic magnetic field with several cusps. Previous studies have indicated that the basic ionization and acceleration processes are directly related to the electron motion behavior, which mainly depends on the magnetic field characteristics. The magnet number and magnet stage length are two key magnetic field parameters that have important effects on the thruster performances. In this paper, both the magnet number and magnet stage length parameters are studied for the optimization of a 5 kW multi-cusped field thruster. The results indicate that the three-stage thruster has a better electron confinement than the two-stage thruster. It has lower ion energy loss at the wall, and shows a higher ionization rate. Therefore, the three-stage magnetic field is a superior magnetic field configuration. Besides, the three-stage magnetic field simulation results indicate that an optimal accelerating electric field distribution and ionization region distribution could be obtained when the magnet length ratio is 78:25:20.
  • loading

Catalog

    Turn off MathJax
    Article Contents

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return