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A demonstration program plan utilizing composite reinforced metals for the DC-8 horizontal stabilizer structure Final reportFeasibility of boron-epoxy reinforced aluminum alloy for horizontal stabilizer structure of DC 8 aircraft and recommendations for demonstration program
Document ID
19710018188
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sumida, P. T.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Subject Category
Aircraft
Report/Patent Number
MDC-J5119
NASA-CR-111913
Report Number: MDC-J5119
Report Number: NASA-CR-111913
Accession Number
71N27664
Funding Number(s)
CONTRACT_GRANT: NAS1-9953
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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