Methods of achieving crash-worthiness of aircraft in general are discussed. Specific conclusions are drawn with regard to the design loads for occupant restraint systems. A “ programmed break” concept for the fuselage of large aircraft is presented, and additional research which is needed to provide increased survival in accidents is suggested.


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    Title :

    Safety Engineering for Crash Injury Prevention


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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