A laboratory test was performed on a model A-6A airframe to determine whether the airframe could sustain the arrestment loads associated with 2000 arrestments at an increased gross weight of 36,000 pounds. The Navy Model NEA6-A, BUNO 149935, used as a test speciment, sustained 4000 arrestment test cycles with no major failures satisfying a service life of 2000 arrestments at a gross weight of 36,000 pounds. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Arrested Landing Fatigue Test of the Model A-6A Aircraft


    Beteiligte:
    H. D. Lystad (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch