Compression creep tests were performed on fully dense speci-I. Introduction mens of UC,.o,, UC,.,,, UCI.,,+4 wt% W, and Uo.gZro., Cl.01+4 wt% W. Steady-state creep rates were measured from 1400" to 1800°C in a vacuum of 1.33 x N/mZ (1 x torr) at stresses of 4.55 to 69.0 MN/m2 (660 to 10, OOO psi). The data for UCl,ol could best be fit by an expression of the form d = 17730s.024 exp (106.5/RT), where i. is the steady-state creep rate (h-l), m is the applied stress (MN/m2), and the creep activation energy is given in kcal/mol. The stress dependence for creep of UC decreased with decreasing temperature because of second-phase. precipitation; therefore, a unique creep activation energy could not be established for this U/C ratio. At all temperatures, the creep strength of UC,.,, exceeded that of UC,.,,. For example, at 1700°C steady-state creep rates for UC1.05 are =YI those for UC,,,,, but at 1400°C the creep rates are = 3 orders of magnitude less. At 1700"C, creep rates for UC alloys are =4 orders of magnitude lower than those for unalloyed UCl,ol.HE creep properties of 4 UC-based fuels were determined as T a function of stress from 1400" to 1800°C. The materials were(1) unalloyedUC,.,,, (2) unalloyedUC,,,,, (3) UC+4 wt% W, and Uranium carbide has the NaCl structure and a melting temperature of 2400"?50°C.1 Its homogeneity range, whose width varies with temperature, extends from =4.75 to4.90 wt% C for temperatures from 1300" to 1900"C, with the stoichiometric composition corresponding to 4.80 wt% C.z Below 4.8 wt% C, U forms in the microstructure after the UC cools to room temperature; above 4.8 wt% C, U2C, or UC2 forms in the microstructure.(4) Uo.g~o.iCi,ni+4 wt% W. Fig. 1. Microstructures of 100%-dense as-cast carbide specimens ( x 250). (A) UC,.,,, ( B ) UC,.,,, (C) UC1,,,+4 wt% W, and (0)Uo.gZro.lCl,ol+4 wt% W.138