Statistical analyses methodologies, such as analysis of variance, non-parametric tests and hypothesis tests were applied to uncover trends and dependencies of ejection-related injuries. Ejection-related fatality patterns for the A-6 aircraft were developed deterministically. The A-4, A-5, A-6, A-7, F-4, F-8 and F-9 ejection-related injuries were investigated, and parent probability density functions derived. The A-4, A-6, A-7, F-4 and F-8 contain an underlying injury trend. Fatalities occur randomly upon ejection from the A-4, A-7, F-4 and F-8 aircraft. Fatalities do not occur randomly from the A-6 aircraft. Differences were revealed among various ejection fatality scenarios: hardware hazards, aircrew judgment, environmental conditions, aircraft associated with ejections, and ejection seats used in ejection. (Author)


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    Titel :

    Statistical Analyses Applied to the U. S. Navy Aircrew Automated Escape Systems


    Beteiligte:
    H. L. Crowson (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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