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Space Shuttle Stiffener Ring Foam Failure Analysis, a Non-Conventional ApproachThe Space Shuttle Program made use of the excellent properties of rigid polyurethane foam for cryogenic tank insulation and as structural protection on the solid rocket boosters. When foam applications de-bond, classical methods of failure analysis did not provide root cause of the failure of the foam. Realizing that foam is the ideal media to document and preserve its own mode of failure, thin sectioning was seen as a logical approach for foam failure analysis to observe the three dimensional morphology of the foam cells. The cell foam morphology provided a much greater understanding of the failure modes than previously achieved.
Document ID
20150023602
Acquisition Source
Kennedy Space Center
Document Type
Abstract
Authors
Howard, Philip M.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Date Acquired
December 31, 2015
Publication Date
August 2, 2015
Subject Category
Nonmetallic Materials
Spacecraft Design, Testing And Performance
Report/Patent Number
KSC-E-DAA-TN20712
Report Number: KSC-E-DAA-TN20712
Meeting Information
Meeting: Microscopy & Microanalysis 2015 Meeting (M&M 2015)
Location: Portland, OR
Country: United States
Start Date: August 2, 2015
End Date: August 6, 2015
Sponsors: Microscopy Society of America
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
cryogenic tank insulation
rigid polyurethane foam
Failure analysis
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