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Program for establishing long-time flight service performance of composite materials in the center wing structure of C-130 aircraft. Phase 3: FabricationThe manufacturing plan for three C-130 aircraft center wing box test articles, selectively reinforced with boron-epoxy composites, is outlined for the following tasks: (1) tooling; (2) metal parts fabrication: (3) reinforcing laminate fabrication; (4) laminate-to-metal parts bonding; and (5) wing box assembly. The criteria used for reliability and quality assurance are discussed, and several solutions to specific manufacturing problems encountered during fabrication are given. For Vol. 1, see N73-13011; for Vol. 2, see N73-22929.
Document ID
19750003865
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harvill, W. E. (Lockheed-Georgia Co. Marietta, GA, United States)
Kays, A. O. (Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
LG74ER0145
NASA-CR-132495
Report Number: LG74ER0145
Report Number: NASA-CR-132495
Accession Number
75N11937
Funding Number(s)
CONTRACT_GRANT: NAS1-11100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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