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Efficient Nondestructive Evaluation of Prototype Carbon Fiber Reinforced StructuresThermography and shearography methods of inspection rely on optic based technologies and can reduce the time and cost required to inspect composite tanks or aerostructures. Usually areas identified as suspect in the initial inspection results are reexamined with ultrasonic methods. This combination of techniques results in a rapid and comprehensive inspection of composite structures. Development of useful defect standards will be discussed. Examples of application of this inspection philosophy to prototype, GSE, and flight hardware will be presented. Methods organizing the inspection and evaluating the results will be considered.
Document ID
20020068103
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Russell, Samuel S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Walker, James
(NASA Marshall Space Flight Center Huntsville, AL United States)
Thom, Robert
Date Acquired
August 20, 2013
Publication Date
January 1, 2002
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: 2002 Assurance Technology Conference
Location: Cleveland, OH
Country: United States
Start Date: May 29, 2002
End Date: May 30, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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