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Thermal effects on fiber optic strain sensors embedded in graphite-epoxy compositesSmart structures deployed in low earth orbit will be exposed to a hostile environment which will include temperature extremes during each orbit as the platform moves from the day to the night side. The stresses due to thermal cycling may compromise the performance of embedded fiber optic strain sensors because of differential thermal expansion of the fiber and the composite material. The effects of elevated temperature and thermal cycling on the performance of a fiber optic strain sensor embedded in a graphite-epoxy tube have been investigated for temperatures from 65 to 220 F. The results indicate that the fiber optic strain sensor measurements correlate well with conventional resistance strain gages attached to the tube.
Document ID
19900045839
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rogowski, R. S.
(NASA Langley Research Center Hampton, VA, United States)
Holben, M. S., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Heyman, J. S.
(NASA Langley Research Center Hampton, VA, United States)
Dehart, D. W.
(USAF, Astronautics Laboratory, Edwards AFB CA, United States)
Margulies, Susan
(AS&M, Inc. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Instrumentation And Photography
Accession Number
90A32894
Distribution Limits
Public
Copyright
Other

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