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Tunable Laser Development for In-flight Fiber Optic Based Structural Health Monitoring SystemsThe 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. This is the regular update of the Tunable Laser Development for In-flight Fiber Optic Based Structural Health Monitoring Systems website.
Document ID
20140008542
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 27, 2014
Publication Date
January 1, 2014
Subject Category
Spacecraft Instrumentation And Astrionics
Lasers And Masers
Report/Patent Number
DFRC-E-DAA-TN13499
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Composite Materials
Fiber Optic Sensors
Structural Health Monitoring

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