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Some space shuttle tile/strain-isolator-pad sinusoidal vibration testsVibration tests were performed on the tile/strain-isolator-pad system used as thermal protection for the space shuttle orbiter. Experimental data on normal and in-plane vibration response and damping properties are presented. Three test specimens exhibited shear type motion during failures that occurred in the tile near the tile/strain-isolator-pad bond-line. A dynamic instability is described which has large in-plane motion at a frequency one-half that of the nominal driving frequency. Analysis shows that this phenomenon is a parametric response.
Document ID
19800021265
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Miserentino, R.
(NASA Langley Research Center Hampton, VA, United States)
Pinson, L. D.
(NASA Langley Research Center Hampton, VA, United States)
Leadbetter, S. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-81853
Report Number: NASA-TM-81853
Accession Number
80N29766
Funding Number(s)
PROJECT: RTOP 506-53-63-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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