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Properties of three graphite/toughened resin compositesResults are presented from an experimental evaluation of IM7/977-2, IM7/F655, and T800/F3900. Data presented include ply-level (unidirectional laminate) strength and moduli, unnotched and notched (open hole) tension and compression properties of quasi-isotropic laminates, and compression-after-impact strengths. These data are compared with properties of other toughened (IM7/8551-7 and IM6/18081) and brittle (T300/5208) graphite-epoxy materials. The IM7/977-2, IM7/F655, and T800/F3900 materials are substantially stronger and more damage tolerant than widely used first generation composite materials such as T300/5208. The T800/F3900 outperforms IM7/977-2 and IM7/F655 materials in tolerance to projectile impacts. Compression-after-impact strengths were found to be dependent on impactor velocity for a given impact energy. The open hole compression properties of all three materials are degraded by the combination of heat and moisture.
Document ID
19920000849
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Smith, Donald L.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Dow, Marvin B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NASA-TP-3102
L-16910
NAS 1.60:3102
Report Number: NASA-TP-3102
Report Number: L-16910
Report Number: NAS 1.60:3102
Accession Number
92N10067
Funding Number(s)
PROJECT: RTOP 505-63-50-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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