• DocumentCode
    951503
  • Title

    Plasma Propulsion Devices for Space Flight

  • Author

    Camac, M. ; Kantrowitz, A. ; Petschek, H.E.

  • Author_Institution
    Avco Everett Research Lab., Everett, Mass.
  • Issue
    2
  • fYear
    1959
  • fDate
    4/1/1959 12:00:00 AM
  • Firstpage
    34
  • Lastpage
    41
  • Abstract
    An analysis of some of the more immediate space missions indicates that a large increase in payload can be achieved when electrical propulsion is used instead of chemical propulsion. For missions in the gravitational field of the Earth and to the Moon, the optimum specific impulse range for electrical propulsion is from about 1500 to 5000 seconds. Electrical propulsion with neutral plasma devices operate well in this specific impulse range as well as at higher specific impulses. Three different chambers have been described as examples of devices using neutral plasmas. Some of the factors which limit the range of efficient operation of such devices have been discussed.
  • Keywords
    Aerospace electronics; Artificial satellites; Chemical analysis; Earth; Moon; Payloads; Plasma devices; Propulsion; Rockets; Space missions;
  • fLanguage
    English
  • Journal_Title
    Military Electronics, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-2511
  • Type

    jour

  • DOI
    10.1109/IRET-MIL.1959.5008131
  • Filename
    5008131