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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    Titel :

    FRAGILITY RATING: (AID TO PACKAGE DESIGN)


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1955




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Fragility rating

    Skidmore, W.H. | Engineering Index Backfile | 1955



    Cushion design from fragility rating

    Nietsch, H.E. | Engineering Index Backfile | 1955


    Cushion Design From Fragility Rating

    Nietsch, H. E. | SAE Technical Papers | 1956


    Fragility

    Safford, F. B. | SAE Technical Papers | 1961