The development of superior-strength materials used in high temperature applications is necessary for the continued improvement of turbine engine systems. Orthorhombic-based intermetallic alloys, such as Ti-25Al-17Nb (at%), have displayed excellent intermediate-temperature strength [1] and creep resistance [2]. However, further improvement in creep behavior may be obtained by altering the microstructure. The addition of molybdenum (Mo), a beta-phase stabilizer, affects the grain size and the constituent phase volume fractions. Small Mo additions of 1 at% have all resulted in significant creep property improvements [3][4][5]. In this work, we evaluated the effect of Mo contents ranging between 0.66 -2.3 Mo on the microstructure and creep behavior of a Ti-24Al-17Nb (at %) alloy. In addition, we evaluated the effect of such Mo contents on the microstructure and creep behavior of Ti-25Al-17Nb-XMo matrices which were reinforced with approximately 37 volume percent continuous silicon carbide fibers.The microstructures of Ti-24Al-17Nb-0.66Mo and Ti-24Al-17Nb-2.25Mo (at %) alloys were analyzed using a Camscan 44FE field emission scanning electron microscope. Increases in Mo concentration led to a decrease in the hexagonal close packed (hcp) α 2 phase volume fraction and an associated increase in orthorhombic and body centered cubic (bcc) phase volume fraction, as shown in Fig. 1. The volume fractions of the Ti-24Al-17Nb-0.66Mo alloy were 38.3% α 2 and 61.7 O + bcc. For the Ti-24Al-17Nb-2.25Mo alloy they were 24.1% α 2 and 75.9% O + bcc.The affect of Mo content on creep behavior was analyzed at temperatures ranging from 650°C to 710°C and stresses ranging from 30 -275 MPa. The Ti-24Al-17Nb-2.25Mo alloy exhibited superior creep resistance compared with the Ti-24Al-17Nb-0.66Mo alloy, as shown in Fig. 2(b). In fact, approximately one order of magnitude difference in minimum creep rate was observed at all stresses evaluated at 650°C. Thus, small changes in Mo concentration significantly affect the creep behavior of Ti-Al-Nb alloys. Using an Ernest Fullam tensile stage, samples were imaged in-situ during the creep experiment. From such experiment, the deformation in the form of cracking was observed at α 2 grain boundaries, see Fig. 2(a). Thus, reducing the continuity and size of the α 2 phase through the addition of small amounts of Mo can have a significant effect on the creep behavior. This trend will be investigated in the metal matrix composite samples, which will be evaluated with the fiber direction both perpendicular and parallel to the loading direction.