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Development and demonstration of manufacturing processes for fabricating graphite/PMR-15 polyimide structuresThe work included establishing controls on the polymer, the prepreg, composite fabrication, and quality assurance, as well as fabrication of structural elements to demonstrate the developed materials and processes. The fabricated structures were hat sections, I-beam sections, honeycomb sandwich structures, and molded graphite-reinforced fittings. The graphite/PMR-15 polyimide system was shown to be well suited for use in the 550-600 F temperature range; the processing techniques developed were proved and found potentially useful for other commercially available systems.
Document ID
19800050585
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Sheppard, C. H.
(Boeing Aerospace Co. Seattle, WA, United States)
Hoggatt, J. T.
(Boeing Aerospace Co. Seattle, WA, United States)
Hunter, A. B.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
Mechanical Engineering
Meeting Information
Meeting: New horizons - Materials and processes for the eighties
Location: Boston, MA
Start Date: November 13, 1979
End Date: November 15, 1979
Accession Number
80A34755
Funding Number(s)
CONTRACT_GRANT: NAS1-15009
Distribution Limits
Public
Copyright
Other

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