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Hypersonic cruise vehicle wing structure evaluation - Volume 2, sections 11-22Structure size, weight, flutter, fatigue, creep, and heat shield analyses for hypersonic cruise vehicle wing
Document ID
19700017939
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davis, G. W. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Plank, P. P. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Richie, C. C. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Sakata, I. F. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 15, 1970
Subject Category
Aircraft
Report/Patent Number
NASA-CR-66897-2
Report Number: NASA-CR-66897-2
Accession Number
70N27249
Funding Number(s)
CONTRACT_GRANT: NAS1-7573
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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