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Nicalon/siliconoxycarbide ceramic composites

Authors :
Hurwitz, F. I
Gyekenyesi, J. Z
Conroy, P. J
Rivera, A. L
Source :
Ceramic Engineering and Science Proceedings. 11
Publication Year :
1990
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1990.

Abstract

A number of polymers of differing molecular structure, viscosity, copolymer composition, and production procedures, screened for production of strong, tough Nicalon/siliconoxycarbide composites, are discussed. Variables during polymer synthesis include pH, water/methoxy ratio and phenyl/methyl ratio. Final processing temperatures of the composites range from 1200 deg to 1400 deg C. The filler is derived from pyrolysis of the 50 phenyl/50 methyl silsesquioxane copolymer pyrolyzed to 650 deg C, then milled to less than 1-micron powder. Composite samples were fractured to evaluate the influence of matrix composition, final fabrication temperature, and use of filler on the composite mode of failure, modulus, strain capability, and strength. Incorporation of filler was found to increase matrix compressive strength and to influence matrix shrinkage and cracking.

Subjects

Subjects :
Composite Materials

Details

Language :
English
ISSN :
01966219
Volume :
11
Database :
NASA Technical Reports
Journal :
Ceramic Engineering and Science Proceedings
Publication Type :
Report
Accession number :
edsnas.19900064869
Document Type :
Report