An experiment has been developed to examine the behavior of a titanium-water loop heat pipe under standard and elevated acceleration fields. The loop heat pipe was mounted on a 2.44 meter-diameter centrifuge table on edge with heat applied to the evaporator via a mica heater and heat rejected using a high-temperature polyalphaolefin oil coolant loop. The loop heat pipe was tested under the following parametric ranges: heat load at the evaporator 100 Q in 600 W, heat load at the compensation chamber 0 Q cc 50 W, radial acceleration 0 a r 10 g. For stationary operation, the evaporative heat transfer coefficient decreased monotonically with heat load whereas the thermal resistance decreased to a minimum then increased. Heat input to the compensation chamber was found to increase the evaporative heat transfer coefficient and decrease the thermal resistance for Q in 500 W. Transient periodic flow reversal in the loop heat pipe was found for some cases, which was likely due to vapor bubble formation in the primary wick. Operation in an elevated acceleration environment revealed that dry out was dependent on both Q in and a r , and the ability for the loop heat pipe to reprime after an acceleration event that induced dry out was influenced by the evaporator temperature. The evaporative heat transfer coefficient and thermal resistance were found not to be significantly dependent on radial acceleration. However, the evaporator wall superheat was found to increase slightly with radial acceleration at high heat loads. Nomenclature a = acceleration, m=s 2 C p = specific heat, J=kg-K D = diameter, m f = frequency, Hz g = standard acceleration, 9:81 m=s 2 h = heat transfer coefficient, W=m 2 -K k = thermal conductivity, W=m-K L = length, m m = mass, kg Nu = Nusselt number, hD=k Q = heat transfer rate, W R = thermal resistance, K=W Ra = Rayleigh number, gT s T 1 D 3 = r = radial coordinate, m T = temperature, K T = average temperature, K t = time, s V = volume, m 3 , voltage, volt = thermal diffusivity, m 2 =s = volumetric thermal expansion coefficient, K 1 = ratio of specific heats T = temperature difference, K T sh = evaporator wall superheat, T e T e=cc , K " = emissivity = resultant acceleration vector angle, arc degrees = absolute viscosity, N-s=m 2 = kinematic viscosity, m 2 =s = density, kg=m 3 = Stefan-Boltzmann constant, 5:67 10 8 W=m 2 -K 4 ' = fluid phase Subscripts amb = ambient b = bayonet inlet c = condenser cc = compensation chamber cl = centerline conv = convection cp = cold plate D = diameter e = evaporator eg = ethylene glycol e=cc = evaporator/compensation chamber junction ie = loop heat pipe inner edge in = in max = maximum oe = loop heat pipe outer edge out = out PAO = polyalphaolefin r = radial rad = radiation sh = superheat tot = total v = vapor z = axial 1 = primary 2 = secondary