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Development and Ground-Test Validation of Fiber Optic Sensor Attachment Techniques for Hot Structures ApplicationsFiber Optic Strain Measurements: a) Successfully attached silica fiber optic sensors to both metallics and composites; b) Accomplished valid EFPI strain measurements to 1850 F; c) Successfully attached EFPI sensors to large scale hot-structures; and d) Attached and thermally validated FBG bond and epsilon(sub app). Future Development a) Improve characterization of sensors on C-C and C-SiC substrates; b) Apply application to other composites such as SiC-SiC; c) Assist development of interferometer based Sapphire sensor currently being conducted under a Phase II SBIR; and d) Complete combined thermal/mechanical testing of FBG on composite substrates in controlled laboratory environment.
Document ID
20060013508
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Piazza, Anthony
(NASA Dryden Flight Research Center Edwards, CA, United States)
Hudson, Larry D.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Richards, W. Lance
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Electronics And Electrical Engineering
Meeting Information
Meeting: SensorsGov Expo and Conference
Location: Hampton, VA
Country: United States
Start Date: December 6, 2005
End Date: December 8, 2005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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