High-Density Helicon Plasma Thrusters Using Electrodeless Acceleration Schemes

DOI Web Site 被引用文献3件 オープンアクセス
  • KUWAHARA Daisuke
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • SHINOHARA Shunjiro
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • ISHII Takamichi
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • OTSUKA Shuhei
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • NAKAGAWA Toshiki
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • KISHI Kensuke
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • SAKATA Marie
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • TANAKA Eiko
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • IWAYA Hiraku
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • TAKIZAWA Kohei
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • TANIDA Yuriko
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • NAITO Takayuki
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
  • YANO Kazuki
    Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology

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<p>We have been studying long-lifetime helicon plasma thrusters as the Helicon Electrodeless Advanced Thruster (HEAT) project. Two important elements of the proposed helicon plasma thruster are a generation of a dense source plasma using a helicon wave, and an acceleration of the plasma by the Lorentz force using the product of the induced azimuthal current and static radial magnetic field. Here, in order to eliminate damage of electrodes, both generation and acceleration schemes are operated in non-contact condition between the plasma and electrodes. Acceleration schemes use two type of coils: rotating magnetic field coils and azimuthal mode number m = 0 ones. These studies have been carried out on the Large Mirror Device (LMD), which has two types the magnetic field source, permanent magnets and electromagnets, and the Small Helicon Device (SHD), which has small diameter discharge tubes. In this paper, current performances of acceleration schemes are reported.</p>

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