Tension strength of a thick graphite/epoxy laminate after impact by a 1/2-in. radius impactor

NASA is developing graphite/epoxy filament-wound cases for solid rocket motors of the space shuttle. They are wet-wound with AS4W graphite fiber and HBRF-55A epoxy. The membrane region is about 1.4 inches thick. Two 30-inch-diameter by 12-inch-long cylinders were impacted every two inches of circumf...

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Bibliographische Detailangaben

Hauptverfasser:	Poe, C. C., Jr, Illg, W., Garber, D. P.
Format:	Report
Sprache:	eng
Schlagworte:	Composite Materials
Online-Zugang:	Volltext bestellen
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