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Study of low-cost fabrication methods for aerospace composite materialsFlat and hat section specimens of graphite/epoxy composite materials have been fabricated by the resin bath or wet pultrusion process. This demonstrated the feasibility of incorporating crossplied graphite fiber reinforcements in conjunction with epoxy resin systems in the wet pultrusion process. However, the thickness constraints of the pultrusion process, the lack of dimensional stability of the crossply materials and equipment limitations affect the quality of the hat section pultrusions. The wet pultrusion process shows promise of being a low cost method for producing composite parts with constant cross section along the length. A cost analysis showed at least 80 percent cost reduction for the hat section and 40 percent for flat panel by pultrusion over the conventional manual and automated lay-up.
Document ID
19780011262
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chung, H. H.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-145330
LR-28308
Report Number: NASA-CR-145330
Report Number: LR-28308
Accession Number
78N19205
Funding Number(s)
CONTRACT_GRANT: NAS1-14730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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