Sets of missiles were subjected to two 10-min vibration tests under combined temperature-altitude environment; temperature ranged from 180F to -30F, and altitude was 40,000 ft; missile was checked for acceptable operation before, during, and after environmental test; missiles which operated satisfactorily after laboratory tests were satisfactory in flight tests; missiles which showed early laboratory test failures and were subsequently corrected, were also satisfactory in flight test; there was good correlation between laboratory tests and flight tests, to indicate value for debugging tests.


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    Title :

    Elimination of substandard parts by environmental testing


    Additional title:

    U S Naval Research Laboratory -- Shock Vibration Bul


    Contributors:


    Publication date :

    1966


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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