With properties lying between those of metals and ceramics, intermetal
lic compounds are particularly attractive for high temperature structu
ral applications. Considerable progress has been made in improving the
ductility of these rather brittle materials, especially with the tita
nium aluminides Ti3Al (alpha-2) and TiAl (gamma). But monolithic inter
metallic compounds are unlikely to have the right combination of ambie
nt temperature ductility and high temperature strength for the most de
manding aeroengine applications. Further progress depends on the devel
opment of engineered composite materials, which exploit the combined p
otential of ceramics, intermetallics and metals to give a desirable ba
lance of properties. This paper reviews developments in intermetallic
matrix composites (IMCs), concentrating on the last four years and dra
wing examples from the three most widely researched matrix systems: ti
tanium aluminides, nickel aluminides and molybdenum disilicide.