System employed in development of Navy's supersonic F11F-1 airplane; objective was to provide reliable, light weight, automatic method of close center of gravity travel independent of electric power; aim achieved through use of hydromechanical devices which utilize compressor bleed air from jet engine as muscle force; advantages.


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    Title :

    Fuel balance system for supersonic airplanes


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Karanik, J. (author)

    Conference:

    Society of Automotive Engineers -- Meeting ; 1956 Supersonic speeds



    Publication date :

    1956


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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