Filament-wound, continuous cross-section, aircraft tire is discussed; requirements for improved tires, and advantages and potential of new design are discussed; results of qualification, dynamometer tests of military tire specification indicate that filament-wound tire of equal strength weighs 15% less than conventional tire; discussions concerning use of automation methods, advanced tire materials, and possible spin-off applications. (12693)


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    Title :

    Development of filament-wound aircraft tires


    Additional title:

    Soc Aerospace Matl and Process Engrs Nat Symp


    Contributors:

    Conference:

    12th SAMPE National Symposium -- Advances in Structural Composites ; 1967 Tires



    Publication date :

    1967


    Size :

    24 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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