• DocumentCode
    447722
  • Title

    Application of high power millimeter-wave to space propulsion

  • Author

    Oda, Y. ; Ushio, M. ; Komurasaki, K. ; Takahashi, K. ; Kasugai, A. ; Sakamoto, K.

  • Author_Institution
    Dept. of Adv. Energy, Tokyo Univ., Chiba, Japan
  • Volume
    1
  • fYear
    2005
  • fDate
    19-23 Sept. 2005
  • Firstpage
    30
  • Abstract
    A microwave beaming thruster boosted by a 170GHz gyrotron was investigated. Plasma was successfully initiated by focusing the millimetre wave beam using a parabolic reflector. The plasma propagation velocity was increased with the beam power density; the velocity became supersonic at the power density beyond 80 kW/cm2. Propulsive impulse was measured through the flight experiments, and resulting momentum coupling coefficient, a ratio of thrust to input energy, was found drastically increased when the plasma propagation velocity becomes supersonic.
  • Keywords
    aerospace propulsion; aerospace testing; gyrotrons; 170 GHz; beam power density; gyrotron; high power millimeter-wave; microwave beaming thruster; millimetre wave beam; momentum coupling coefficient; parabolic reflector; plasma propagation velocity; propulsive impulse; space propulsion; supersonic velocity; Energy measurement; Gyrotrons; Microwave propagation; Millimeter wave propagation; Particle beams; Plasma applications; Plasma density; Plasma measurements; Plasma waves; Propulsion;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Infrared and Millimeter Waves and 13th International Conference on Terahertz Electronics, 2005. IRMMW-THz 2005. The Joint 30th International Conference on
  • Print_ISBN
    0-7803-9348-1
  • Type

    conf

  • DOI
    10.1109/ICIMW.2005.1572391
  • Filename
    1572391