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NASA NTRS · 19910022871

Materials and processes laboratory composite materials characterization task, part 1. Damage tolerance

Abstract

A 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.

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BibTeXRIS

Nettles, A. T., Tucker, D. S., Patterson, W. J., Franklin, S. W., Gordon, G. H., Hart, L., Hodge, A. J., Lance, D. G., Russel, S. S.. 1991-09-01. Materials and processes laboratory composite materials characterization task, part 1. Damage tolerance. https://ntrs.nasa.gov/citations/19910022871

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