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Space Shuttle Stiffener Ring Foam Failure Analysis, a Non-Conventional Approach.The 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
20180004521
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Howard, Philip M.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 17, 2018
Publication Date
April 20, 2018
Subject Category
Quality Assurance And Reliability
Spacecraft Design, Testing And Performance
Report/Patent Number
STI 18733
KSC-E-DAA-TN54921
KSC-E-DAA-TN20712
KSC-E-DAA-TN24400
KSC-MSL-2007-0136
Meeting Information
Meeting: Rutgers University NASA Panel
Location: New Brunswick, NJ
Country: United States
Start Date: April 20, 2018
Sponsors: Rutgers Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Foam
failure analysis
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