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Assessment of Technologies for the Space Shuttle External Tank Thermal Protection System and Recommendations for Technology Improvement - Part 2: Structural Analysis Technologies and Modeling PracticesA technology review and assessment of modeling and analysis efforts underway in support of a safe return to flight of the thermal protection system (TPS) for the Space Shuttle external tank (ET) are summarized. This review and assessment effort focuses on the structural modeling and analysis practices employed for ET TPS foam design and analysis and on identifying analysis capabilities needed in the short-term and long-term. The current understanding of the relationship between complex flight environments and ET TPS foam failure modes are reviewed as they relate to modeling and analysis. A literature review on modeling and analysis of TPS foam material systems is also presented. Finally, a review of modeling and analysis tools employed in the Space Shuttle Program is presented for the ET TPS acreage and close-out foam regions. This review includes existing simplified engineering analysis tools are well as finite element analysis procedures.
Document ID
20040129726
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Norman F Knight, Jr
(General Dynamics (United States) Reston, United States)
Michael P Nemeth
(Langley Research Center Hampton, United States)
Mark W Hilburger
(Langley Research Center Hampton, United States)
Date Acquired
August 22, 2013
Publication Date
August 1, 2004
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/TM-2004-213256/PT2
L-19044/PT2
LF99-807
Funding Number(s)
WORK_UNIT: 23-794-40-4M
CONTRACT_GRANT: GSA-GS-00F-0067M
TASK: NASA Order L-71395-D
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
External tank foam
Space Shuttle
Thermal protection
Foam
Structural analysis verification and validation
Acceptance criteria
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