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Accession Number:
AD0269336
Title:
DEVELOPMENT OF IMPROVED HIGH-STRENGTH PREIMPREGNATED MATERIALS FOR FILAMENT-WOUND ROCKET MOTOR CASES
Corporate Author:
AEROJET-GENERAL CORP AZUSA CALIF
Report Date:
1961-12-18
Abstract:
Test were made on experimental glass for both dry glass and pre-preg for Lot 1 and the control glass Lot 37. Lots 1 and 3 of experimental glass had strand tensile strengths of over 340,000 psi, which is more than 10 higher than for the control glass. NOL-ring and chamber test results were about the same for both pre-preg and dryglass versions of the experimental and control glasses. Author
Pages:
0006
Contract Number:
NOw-61-0642
File Size:
0.00MB
