An SiC-particulate, silicon-metal melt-infiltration-matrix composite reinfo
rced with SiC fibers is being developed for combustor applications under th
e High Speed Civil Transport (HSCT) Enabling Propulsion Material (EPM) Prog
ram. A major part of this effort has dealt with the characterization and op
timization of the boron nitride (BN) based fiber/matrix interface. BN was c
hosen as the primary interfacial material due to its inherently weak struct
ure and thus good crack-deflecting ability, ease of deposition by chemical
vapor infiltration (CVI) into woven fiber preforms, and relatively good env
ironmental stability. Topics discussed in this paper include an overview of
the differences in composite microstructure between the EPM SiC/SiC materi
al and a more conventional CVI SiC/SiC composite material, the microstructu
re/property relationships for the EPM SiC/SiC composite with two different
types of SiC fiber (High-Nicalon and Sylramic(TM)), and the effect of moist
, high-temperature environments on the stability of the BN interface. (C) 2
000 Acta Metallurgica Inc. Published by Elsevier Science Ltd. AII rights re
served.