Propellant actuated devices, originally developed for use in conventional aircraft, were subjected to special vibration tests in order to qualify them for use in the Dyna-Soar (X20) Escape System. Four initiators were developed for use in the system and the ejection seat catapult was tested under high g loads to determine safety of the defice if initiated during high down-load conditions. (Author)


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    Titel :

    Dyna-Soar Escape System Propellant Actuated Devices


    Beteiligte:
    R. C. Sutter (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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