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Prediction and verification of creep behavior in metallic materials and components for the space shuttle thermal protection system. Volume 3, phase 3: Full size heat shield data correlation and design criteriaAnalysis methods for predicting cyclic creep deflection in stiffened metal panel structures, were applied to full size panels. Results were compared with measured deflections from cyclic tests of thin gage L605, Rene' 41, and TDNiCr full size corrugation stiffened panels. A design criteria was then formulated for metallic thermal protection panels subjected to creep. A computer program was developed to calculate creep deflections.
Document ID
19750025157
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cramer, B. A.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Davis, J. W.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Publication Information
Publisher: NASA
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-132605-3
Report Number: NASA-CR-132605-3
Accession Number
75N33230
Funding Number(s)
CONTRACT_GRANT: NAS1-11774
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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