SYMPOSIA PAPER Published: 01 July 1963
STP44521S

Infrared Nondestructive Testing of Glass Filament-Wound Rocket Motor Cases

Source

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
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Details
Developed by Committee: E07
Pages: 105–114
DOI: 10.1520/STP44521S
ISBN-EB: 978-0-8031-5993-8
ISBN-13: 978-0-8031-6147-4