Methods of achieving crashworthiness of aircraft in general are discussed; specific conclusions are drawn with regard to design loads for occupant restraint systems; "programmed break" concept for 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 -- Proc


    Contributors:

    Conference:

    Proceedings of 3rd Aerospace Reliability and Maintainability Conference ; 1964 Accident prevention


    Published in:

    Publication date :

    1964


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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