Wind tunnel tests and theoretical studies were conducted to determine the feasibility of using the crew compartment of a typical airplane as an escape capsule. The stability characteristics of the separated capsule and the airplane with capsule removed were determined. In order to have a safe separation, the capsule must be forcibly ejected away from the airplane and have a stabilizing device deployed. (Author)


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    Titel :

    A Feasibility Study of an Escape Capsule System for High-Speed Aircraft


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

    Erscheinungsdatum :

    1965


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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