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IMPACT STUDIES ON ABLATION-RESISTANT COMPOSITES,
GENERAL ELECTRIC CO PHILADELPHIA PA MISSILE AND SPACE DIV
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The evaluation of composite configurations by the flying target technique is discussed. The critical impact pressure for epoxy-neoprane foam rubber-aluminum composite was found to be 2.6 kb. The critical impact pressure for pyrolytic graphite surface nucleatedneoprane foam rubber-aluminum composite was also found to be in the range of 2.6 kb. It was established that the substrates have a large influence on the critical impact pressure of the composites. Author
APPROVED FOR PUBLIC RELEASE