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NASA Applications of Structural Health Monitoring TechnologyThis presentation provides examples of research and development that has recently or is currently being conducted at NASA, with a special emphasis on the application of structural health monitoring (SHM) of aerospace vehicles. SHM applications on several vehicle programs are highlighted, including Space Shuttle Orbiter, the International Space Station, Uninhabited Aerial Vehicles, and Expendable Launch Vehicles. Examples of current and previous work are presented in the following categories: acoustic emission impact detection, multi-parameter fiber optic strain-based sensing, wireless sensor system development, and distributed leak detection.
Document ID
20140010525
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Richards, W Lance (NASA Dryden Flight Research Center Edwards, CA United States)
Madaras, Eric I. (NASA Langley Research Center Hampton, VA United States)
Prosser, William H. (NASA Langley Research Center Hampton, VA, United States)
Studor, George (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 8, 2014
Publication Date
September 1, 2013
Subject Category
Quality Assurance And Reliability
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-E-DAA-TN11102
Meeting Information
Meeting: International Workshop on Structural Health Monitoring
Location: Stanford, CA
Country: United States
Start Date: September 10, 2013
End Date: September 12, 2013
Sponsors: Office of Naval Research, Army Research Office, National Science Foundation, Air Force Office of Scientific Research
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Fiber Optic Sensors
Structural Sensing
Acoustic Emission Sensors

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