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Some considerations in the fatigue design of launch and spacecraft structuresMetal fatigue, structural fatigue, and strength for launch vehicle and spacecraft structures
Document ID
19650015673
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bellinfante, R. J. (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Christensen, R. H. (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-242
Report Number: NASA-CR-242
Accession Number
65N25274
Funding Number(s)
CONTRACT_GRANT: NAS7-298
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
METAL FATIGUE
SPACECRAFT STRUCTURE

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