High Power Laser and Particle Beams, Volume. 34, Issue 4, 044005(2022)

Mechanical properties analysis of a 20 cm diameter ion thruster

Kai Shi, Mingming Sun*, Zuo Gu, and Shichao Yue
Author Affiliations
  • National Key Laboratory of Vacuum and Cryogenic Technology on Physics, Lanzhou Institute of Physics, Lanzhou 730070, China
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    Figures & Tables(12)
    Structure of 20 cm diameter ion thruster
    x-direction deformation and Von-Mises stress of different accelerator grid structure
    Components simplification of 20 cm diameter thruster
    Finite element analysis model of LIPS-200 ion thruster
    Pre-stress and pre-deformation of 20 cm ion thruster
    z-direction Von-Mises stress and deformation of the grids under impact load
    z-direction Von-Mises stress and deformation of the grids by elastic support under impact load
    x-direction fundamental frequency and response spectrum
    • Table 1. Effective property of the grids of 20 cm ion thruster

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      Table 1. Effective property of the grids of 20 cm ion thruster

      componentmaterialtransparencyeffective density/(kg·m−3) effective Young’s modulus /GPa Poisson ratio
      the screen gridMo0.69297399.20.31
      the accelerator gridMo0.277001233.60.31
    • Table 2. Comparison of modal analysis for different FEM models of the accelerator grid

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      Table 2. Comparison of modal analysis for different FEM models of the accelerator grid

      structuremodal analysis results of the accelerator grid/Hz
      1st step2nd step3rd step4th step5th step6th step
      with-aperture (reality)51.815207.55251.89303.24427.88474.92
      without-aperture (effective)47.193194.05237.34293.65405.02453.04
    • Table 3. Different components material property of 20 cm ion thruster

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      Table 3. Different components material property of 20 cm ion thruster

      componentsmaterialdensity/(kg·m−3) Young’s modulus/GPaPoisson ratioextension strength/MPa
      mount ring2A122700720.31265
      up/down harness2A122700720.31265
      magnet (effective)4105720.31265
      up/down magnet poleDT47830810.29170
      hollow cathode1Cr18Ni9Ti79301930.31200
      boltsTC-44620960.34825
    • Table 4. Primary 6 step modal frequencies and effective mass percentage of thruster

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      Table 4. Primary 6 step modal frequencies and effective mass percentage of thruster

      modalfrequency/Hzx-direction/% y-direction/% z-direction/%
      1246.0663511
      2248.1671370
      3338.7224050
      4404.4840170
      5411.3241503
      6605.016001
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    Kai Shi, Mingming Sun, Zuo Gu, Shichao Yue. Mechanical properties analysis of a 20 cm diameter ion thruster[J]. High Power Laser and Particle Beams, 2022, 34(4): 044005

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    Paper Information

    Category: Particle Beams and Accelerator Technology

    Received: Sep. 26, 2021

    Accepted: Jan. 28, 2022

    Published Online: Apr. 12, 2022

    The Author Email: Mingming Sun (smmhappy@163.com)

    DOI:10.11884/HPLPB202234.210419

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