Polymer matrix composites offer excellent properties such as high spec
ific strength and stiffness, which make them attractive for many naval
, aerospace, and automotive applications. Although they are candidate
materials for many applications where high strain rate loading is prob
able, little is known of the material responses to shock loading for m
ost composite materials. Because mechanical properties vary significan
tly with strain rate, the use of static properties in the analysis and
design of structures that undergo dynamic loadings can, on one hand,
lead to a very conservative overweight design or, on the other hand, c
an lead to designs that fail prematurely and unexpectedly. The use of
dynamic material properties will ensure the design of composite struct
ures, which are weight efficient and structurally sound when they are
subjected to dynamic loads. A split Hopkinson pressure bar is used to
obtain compressive mechanical properties of Cycom 5920/1583, an uniaxi
al cloth, E-glass/rubber toughened epoxy composite being used presentl
y by the Electric Boat Division of General Dynamics for undersea struc
tures, Yield stress, yield strain, ultimate stress, ultimate strain, a
nd modulus of elasticity values are presented and analyzed wherein the
strain rates vary from 60 to 1150 s(-1).