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Probabilistic Structural Health Monitoring of the Orbiter Wing Leading EdgeA structural health monitoring (SHM) system can contribute to the risk management of a structure operating under hazardous conditions. An example is the Wing Leading Edge Impact Detection System (WLEIDS) that monitors the debris hazards to the Space Shuttle Orbiter s Reinforced Carbon-Carbon (RCC) panels. Since Return-to-Flight (RTF) after the Columbia accident, WLEIDS was developed and subsequently deployed on board the Orbiter to detect ascent and on-orbit debris impacts, so as to support the assessment of wing leading edge structural integrity prior to Orbiter re-entry. As SHM is inherently an inverse problem, the analyses involved, including those performed for WLEIDS, tend to be associated with significant uncertainty. The use of probabilistic approaches to handle the uncertainty has resulted in the successful implementation of many development and application milestones.
Document ID
20110008039
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Yap, Keng C.
(Boeing Space Exploration Houston, TX, United States)
Macias, Jesus
(United Space Alliance Huntsville, AL, United States)
Kaouk, Mohamed
(NASA Johnson Space Center Houston, TX, United States)
Gafka, Tammy L.
(NASA Johnson Space Center Houston, TX, United States)
Kerr, Justin H.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Structural Mechanics
Meeting Information
Meeting: 19th Adaptive Structures Conference
Location: Denver, CO
Country: United States
Start Date: April 4, 2011
End Date: April 7, 2011
Funding Number(s)
CONTRACT_GRANT: 6000131279
Distribution Limits
Public
Copyright
Public Use Permitted.
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