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Fabrication of graphite/polyimide composite structures.Selection of graphite/polyimide composite as a prime candidate for high-temperature structural applications involving long-duration temperature environments of 400 to 600 F. A variety of complex graphite/polyimide components has been fabricated, using a match-metal die approach developed for making fiber-reinforced resin composites. Parts produced include sections of a missile adapter skin flange, skin frame section, and I-beam and hat-section stringers, as well as unidirectional (0 deg) and plus or minus 45 deg oriented graphite/polyimide tubes in one-, two-, and six-inch diameters.
Document ID
19730035646
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
Varlas, M.
(General Dynamics Corp. Convair Aerospace Div., San Diego, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
SME PAPER EM 72-107
Accession Number
73A20448
Funding Number(s)
CONTRACT_GRANT: NAS8-26198
Distribution Limits
Public
Copyright
Other

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