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Structural Health Monitoring Analysis for the Orbiter Wing Leading EdgeThis viewgraph presentation reviews Structural Health Monitoring Analysis for the Orbiter Wing Leading Edge. The Wing Leading Edge Impact Detection System (WLE IDS) and the Impact Analysis Process are also described to monitor WLE debris threats. The contents include: 1) Risk Management via SHM; 2) Hardware Overview; 3) Instrumentation; 4) Sensor Configuration; 5) Debris Hazard Monitoring; 6) Ascent Response Summary; 7) Response Signal; 8) Distribution of Flight Indications; 9) Probabilistic Risk Analysis (PRA); 10) Model Correlation; 11) Impact Tests; 12) Wing Leading Edge Modeling; 13) Ascent Debris PRA Results; and 14) MM/OD PRA Results.
Document ID
20100042148
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Yap, Keng C.
(Boeing Co. Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
December 6, 2010
Subject Category
Avionics And Aircraft Instrumentation
Report/Patent Number
JSC-CN-22129
Meeting Information
Meeting: Joint JANNAF Conference Space Vehicle and Propulsion Systems Wireless Sensors Workshop
Location: Orlando, FL
Country: United States
Start Date: December 6, 2010
End Date: December 10, 2010
Sponsors: Department of the Army, NASA Headquarters, Johns Hopkins Univ., Department of the Navy, Department of the Air Force
Funding Number(s)
OTHER: 6000131279
Distribution Limits
Public
Copyright
Public Use Permitted.
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