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Development of Non Destructive Evaluation Techniques for the In-Situ Inspection of the Orbiter's Thermal Protection SystemOne of the Columbia Accident Investigation Board's (CAB) recommendation is to develop and implement an inspection plan to determine the structural integrity of all Reinforced Carbon-Carbon (RCC) system components that make part of the Space Shuttle's thermal protection system. This presentation focuses on the efforts to leverage non-destructive evaluation (NDE) expertise from academia, private industry, and government agencies resulting in the design of a comprehensive health monitoring program for RCC components. The different NDE techniques that were considered are presented along with the chosen techniques and preliminary inspection results of RCC materials.
Document ID
20050217418
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hernandez, Jose M.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 7, 2013
Publication Date
April 2, 2004
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: IEEE University of Guadalajara Conference
Country: Mexico
Start Date: April 2, 2004
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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