This paper discusses the results of the experimental study that was conducted in order to determine the material properties of a hybrid composite laminate made from Fiberite material MXM-7714/120 (a fabric prepreg consisting of woven Kevlar(R) 49 reinforcement impregnated with Fiberite 250 degrees F (121 degrees C) curing 7714 epoxy resin) and HYE-2448AIE (a 250 degrees F (121 degrees C) curing epoxy resin impregnated unidirectional graphite tape). First, each of the materials that comprise the hybrid laminate was fabricated separately according to ASTM D-3039 specification in order to determine their material properties. The materials were then hybridized and the properties were determined, Data from this experiment reveal that a new class of material that can meet desired specifications can be created through hybridization. The data also revealed that the properties of the materials bonded together as a hybrid complement the properties of the constituent members of the hybrid.