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Development of design data for graphite reinforced epoxy and polyimide compositesProcessing techniques and design data were characterized for a graphite/epoxy composite system that is useful from 75 K to 450 K, and a graphite/polyimide composite system that is useful from 75 K to 589 K. The Monsanto 710 polyimide resin was selected as the resin to be characterized and used with the graphite fiber reinforcement. Material was purchased using the prepreg specification for the design data generation for both the HT-S/710 and HM-S/710 graphite/polyimide composite system. Lamina and laminate properties were determined at 75 K, 297 K, and 589 K. The test results obtained on the skin-stringer components proved that graphite/polyimide composites can be reliably designed and analyzed much like graphite/epoxy composites. The design data generated in the program includes the standard static mechanical properties, biaxial strain data, creep, fatigue, aging, and thick laminate data.
Document ID
19740024871
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Scheck, W. G.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-CR-120413
GDC-DBG70-005
Accession Number
74N32984
Funding Number(s)
CONTRACT_GRANT: NAS8-26198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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