This paper is based on a prior paper by the same author entitled “Fragility Rating For Aircraft Equipment”. The analogy between accelerations caused by vibration and shock is discussed. Testing to establish a fragility rating is discussed and a rating is established for a Klystron based upon tests discussed in a companion paper. Comparative fragility data is presented, showing a wide scope of fragility, size, weight and loading.


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    Title :

    FRAGILITY RATING: (AID TO PACKAGE DESIGN)


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1955-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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