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Structural integrity test and assessment.The feasibility of using an ultrasonic system on board the Space Shuttle Orbiter to facilitate structural evaluation and assessment was studied. Two factors are considered that could limit the capability of an ultrasonic system: (1) the effect of structure configuration and (2) the noise generated during vehicle launch. Results of the study indicate that although the structural configuration has direct bearing on sound propagation, strategic location of transducers will still permit flaw detection. The ultrasonic response data show that a severe acoustic environment does not interfere significantly with either propagation and reflection of surface waves or detection of crack-like flaws in the structure.
Document ID
19720048032
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Suggs, F.
Poe, R.
(North American Rockwell Corp. El Segundo, Calif., United States)
Sannicandro, R.
(NASA Kennedy Space Center Fla., United States)
Date Acquired
August 6, 2013
Publication Date
March 1, 1972
Subject Category
Materials, Metallic
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics and NASA, Space Shuttle Operations, Maintenance, and Safety Technology Conference
Location: Cocoa Beach, FL
Start Date: March 29, 1972
Sponsors: NASA, American Institute of Aeronautics and Astronautics
Accession Number
72A31698
Funding Number(s)
CONTRACT_GRANT: NAS10-7679
Distribution Limits
Public
Copyright
Other

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