Editor's Note: This article describes the composition of metal·matrix composites using a nomenclature system consisting of five parts: the matrix alloy designation, the reinforcement material, the volume percent of the reinforcement, the morphology of the reinforcement, and the generic temper designation. Under this system, a matrix of aluminum alloy 6061 reinforced with 40 vol. % SiC particulate and given a T6 heat treatment is written as 6061 /SiC/ 4Op-T6. When a matrix/reinforcement system is being discussed in general terms, it is deSignated in the same fashion, but a subscript is affixed to the reinforcement material designation to indicate whether it is whisker (w) or particulate (p). Thus, the family of composites formed by reinforcing aluminum alloy 2124 with Si,N. whiskers is designated 2124/Si,N«wl' Superplasticity hos been observed in many aluminum metal-matrix composites at extremely high strain rates (approximately 0.1-1 S-I). These materials generally exhibited a strain-rate sensitivity value of about 0.3 and a maximum elongation of about 300%. It is believed thot the presence ofa liquid phose, or in some cases a low-melting-point region, at the reinforcement/matrix interfaces is responsible for the phenomenon. This phenomenon is not observed in all reinforced composites, despite the fact thot they contain fine grain sizes. Thus, a fine matrix grain size is a necessary but insufficient condition for the high-strain-rate superplasticity.