The investigation was conducted to evaluate the performance of Alcoa AM2 and electron beam welded XM18 landing mat. The test section was subjected to traffic representing 1600 operational cycles of an aircraft having a 60,000-lb gross weight with a single-wheel main-gear assembly load of 27,000 lb and a 30x7.7 tire inflated to 400 psi. (Author Modified Abstract)


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    Title :

    Evaluation of Modifications of AM2 and XM18 Landing Mat


    Contributors:
    C. D. Burns (author) / D. P. Wolf (author)

    Publication date :

    1970


    Size :

    56 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English