Development Policy of a High-Power Millimeter-Wave Oscillator Gyrotron Intended for Microwave Rocket Research

DOI
  • TANIGUCHI Tomohei
    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
  • KOMURASAKI Kimiya
    Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo
  • KARIYA Tuyoshi
    Plasma Research Center, University of Tsukuba
  • MINAMI Ryutaro
    Plasma Research Center, University of Tsukuba
  • IMAI Tuyoshi
    Plasma Research Center, University of Tsukuba
  • ODA Yasuhisa
    Department of Mechanical Engineering, Faculty of Science and Engineering, Setsunan University
  • FUKUNARI Masahumi
    Research Center for Development of Far-Infrared Region, University of Fukui
  • SAKAMOTO Keishi
    National Institutes for Quantum and Radiological Science and Technology

Bibliographic Information

Other Title
  • マイクロ波ロケット研究に向けた大電力ミリ波光源ジャイロトロンの開発方針

Description

<p>  Microwave Rocket obtains an impulsive thrust by utilizing millimeter-wave supported detonation induced by a millimeter-wave beam oscillator, gyrotron. To design a thruster, it is necessary to reproduce its thrust generation process quantitatively. Therefore, in order to conduct detailed measurement on millimeter supported detonation, a new gyrotron, specially designed for atmospheric millimeter-wave discharge, has been developed. This paper summarizes its specifications.</p>

Journal

Details 詳細情報について

  • CRID
    1390565134829111424
  • NII Article ID
    130007799155
  • DOI
    10.24662/sspss.5.0_3
  • ISSN
    24321060
  • Text Lang
    ja
  • Data Source
    • JaLC
    • CiNii Articles
  • Abstract License Flag
    Disallowed

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