• DocumentCode
    951511
  • Title

    Plasma Propulsion Possibilities

  • Author

    Rayle, Warren

  • Author_Institution
    Lewis Res. Center, Natl. Aeronautics and Space Admin., Cleveland, Ohio.
  • Issue
    2
  • fYear
    1959
  • fDate
    4/1/1959 12:00:00 AM
  • Firstpage
    42
  • Lastpage
    45
  • Abstract
    Plasma propulsion systems are arranged in three categories according to the cyclic nature of the jet produced; 1) steady, 2) alternating or wave-accelerated, and 3) pulsed. Typical systems within each category are described with emphasis on work being done at the NASA Lewis Research Center. The criteria for evaluating the relative merits of these systems are listed and the advantages and disadvantages pointed out. Such parameters as energy efficiency and propellant utilization must be measured before conclusions can be reached as to the eventual applicability of any of these systems.
  • Keywords
    Acceleration; Ion beams; Military aircraft; NASA; Plasma accelerators; Plasma devices; Plasma temperature; Plasma waves; Propulsion; Thermal expansion;
  • fLanguage
    English
  • Journal_Title
    Military Electronics, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-2511
  • Type

    jour

  • DOI
    10.1109/IRET-MIL.1959.5008132
  • Filename
    5008132