• DocumentCode
    1502905
  • Title

    Of current interest: Liquid propellant rocket engine for redstone

  • Volume
    77
  • Issue
    2
  • fYear
    1958
  • Firstpage
    190
  • Lastpage
    191
  • Abstract
    MORE THAN 75,000 pounds of thrust is developed by the liquid propellant rocket engine which has been put into production by Rocketdyne, a Division of North American Aviation, Inc., of Canoga Park, Calif., for the U.S. Army´s midrange giant Redstone missile. This is a towering 62-foot rocket weapon measuring 6 feet in diameter.
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1958.6445643
  • Filename
    6445643