Parametric influences of ballistic missile during flight are considered and dynamic environment can be determined in probability terminology of means and extremes; flight vibration characteristics, identified as transient, random or sinusoidal; expected losses in locating pickup for vibration and shock measurements.


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    Title :

    Design of experiment in determination of shock and vibration environment


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1960 Vibrations



    Publication date :

    1960


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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