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Tunable Laser Development for In-Flight Fiber Optic Based Structural Health Monitoring SystemsBriefing based on tunable laser development for in flight fiber optic based structural health monitoring systems. The objective of this task is to investigate, develop, and demonstrate a low-cost swept lasing light source for NASA DFRC's fiber optics sensing system (FOSS) to perform structural health monitoring on current and future aerospace vehicles.
Document ID
20140008320
Acquisition Source
Armstrong Flight Research Center
Document Type
Other
Authors
Richards, Lance (NASA Dryden Flight Research Center Edwards, CA United States)
Parker, Allen (NASA Dryden Flight Research Center Edwards, CA United States)
Chan, Patrick (NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
June 16, 2014
Publication Date
July 25, 2013
Subject Category
Optics
Lasers And Masers
Report/Patent Number
DFRC-E-DAA-TN10290
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Fiber Optic Sensors
Composite Materials
Structural Health Monitoring

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