STP350

    Infrared Nondestructive Testing of Glass Filament-Wound Rocket Motor Cases

    Published: Jul 1963


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    Abstract

    A description of experimental and theoretical studies leadin gto the demonstration of the feasibility of flaw detection in glass filament-wound rocket motor cases, using infrared scanning, is presented. The importance of selecting the best method of heating the specimen in order better to improve the information derived from observation is emphasized. Sources of error are reviewed. The apparatus, measurement techniques, and experimental results are described.


    Author Information:

    Alzofon, Frederick E.
    Lockheed Missiles and Space Co., Sunnyvale, Calif

    Florant, Lester E.
    Lockheed Missiles and Space Co., Sunnyvale, Calif

    Ronald, Richard K.
    Lockheed Missiles and Space Co., Sunnyvale, Calif

    Vann, Marvin J.
    Lockheed Missiles and Space Co., Sunnyvale, Calif

    FItzgerald, Julian E.
    Lockheed Missiles and Space Co., Sunnyvale, Calif


    Paper ID: STP44521S

    Committee/Subcommittee: E07.10

    DOI: 10.1520/STP44521S


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