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Thermal stress analysis of reusable surface insulation for shuttleAn iterative procedure for accurately determining tile stresses associated with static mechanical and thermally induced internal loads is presented. The necessary conditions for convergence of the method are derived. An user-oriented computer program based upon the present method of analysis was developed. The program is capable of analyzing multi-tiled panels and determining the associated stresses. Typical numerical results from this computer program are presented.
Document ID
19740027164
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ojalvo, I. U. (Grumman Aerospace Corp. Bethpage, NY, United States)
Levy, A. (Grumman Aerospace Corp. Bethpage, NY, United States)
Austin, F. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-132502
Report Number: NASA-CR-132502
Accession Number
74N35277
Funding Number(s)
CONTRACT_GRANT: NAS1-10635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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