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Ultrasonic Probing Of Complexly Shaped JointsTechnique developed involves use of ultrasonics to inspect first bond surfaces of solid-rocket-motor joints. By fitting pieces of insulating materials to mate exactly with complicated shapes of affected parts of insulation, complicated shapes redefined into simpler ones probed more easily. When technique used to insonify from insulation side, one readily detects difference between disbond and good bond. Same technique applied to field tang joints, field clevis joints, and aft-dome-to-fixed-nozzle-housing attachment points. Although developed for inspecting joints in solid rocket motors, also applicable to nondestructive evaluation of other complicated joints.
Document ID
19930000585
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Madaras, Eric I.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14626
Accession Number
93B10585
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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