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Space Shuttle Stiffener Ring Foam Failure, a Non-Conventional ApproachThe Space Shuttle makes 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 debond, classical methods of analysis do not always 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. Thin sectioning in two directions, both horizontal and vertical to the application, was chosen 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
20130012565
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Howard, Philip M.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
July 9, 2007
Subject Category
Nonmetallic Materials
Report/Patent Number
KSC-2007-105
Report Number: KSC-2007-105
Meeting Information
Meeting: 59th Inter Micro Conference
Location: Chicago, IL
Country: United States
Start Date: July 9, 2007
End Date: July 12, 2007
Sponsors: McCrone Research Inst.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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