Electron Beam Emission of UT Gyrotron

DOI Open Access
  • MANABE Ayuto
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • TAMAGAWA Toshiyuki
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • TABATA Kuniyoshi
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • TANIGUCHI Tomohei
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • KOMURASAKI Kimiya
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • KARIYA Tsuyoshi
    Plasma Research Center, University of Tsukuba
  • MINAMI Ryutaro
    Plasma Research Center, University of Tsukuba
  • IMAI Tsuyoshi
    Plasma Research Center, University of Tsukuba
  • ODA Yasuhisa
    Department of Mechanical Engineering, Faculty of Science and Engineering, Setsunan University
  • FUKUNARI Masafumi
    Research Center for Development of Far-Infrared Region, University of Fukui
  • YAMAGUCHI Yuusuke
    Research Center for Development of Far-Infrared Region, University of Fukui
  • TATEMATSU Yoshinori
    Research Center for Development of Far-Infrared Region, University of Fukui
  • HAYASHI Kazuo
    National Institutes for Quantum and Radiological Science and Technology
  • IKEDA Ryosuke
    National Institutes for Quantum and Radiological Science and Technology
  • KAJIWARA Ken
    National Institutes for Quantum and Radiological Science and Technology
  • TAKAHASHI Koji
    National Institutes for Quantum and Radiological Science and Technology
  • SAKAMOTO Keishi
    National Institutes for Quantum and Radiological Science and Technology

Bibliographic Information

Other Title
  • 東大ジャイロトロンの電子ビーム引き出し試験

Abstract

<p>  A gyrotron is a vacuum tube which generates millimeter waves from kinetic energy of gyro motion of electrons. In the University of Tokyo, a gyrotron with power of 600 kW, frequency of 94 GHz and pulse duration of 100 microseconds has been developed for the purpose of thrust generation experiments of Microwave Rocket. In order to maximize the energy conversion efficiency, the distribution of magnetic field by the super conducting magnet was measured and the gyrotron was installed. The withstand voltage of 40 kV was confirmed before the beam extraction was examined.</p>

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Details 詳細情報について

  • CRID
    1390850247499971840
  • NII Article ID
    130007996769
  • DOI
    10.24662/sspss.6.0_34
  • ISSN
    24321060
  • Text Lang
    ja
  • Data Source
    • JaLC
    • CiNii Articles
    • KAKEN
  • Abstract License Flag
    Disallowed

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