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Materials and processes laboratory composite materials characterization task, part 1. Damage toleranceA test run was performed on IM6/3501-6 carbon-epoxy in which the material was processed, machined into specimens, and tested for damage tolerance capabilities. Nondestructive test data played a major role in this element of composite characterization. A time chart was produced showing the time the composite material spent within each Branch or Division in order to identify those areas which produce a long turnaround time. Instrumented drop weight testing was performed on the specimens with nondestructive evaluation being performed before and after the impacts. Destructive testing in the form of cross-sectional photomicrography and compression-after-impact testing were used. Results show that the processing and machining steps needed to be performed more rapidly if data on composite material is to be collected within a reasonable timeframe. The results of the damage tolerance testing showed that IM6/3501-6 is a brittle material that is very susceptible to impact damage.
Document ID
19910022871
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nettles, A. T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tucker, D. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Patterson, W. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Franklin, S. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gordon, G. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hart, L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hodge, A. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lance, D. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Russel, S. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-103553
NAS 1.15:103553
Report Number: NASA-TM-103553
Report Number: NAS 1.15:103553
Accession Number
91N32185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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