Gas turbine engines, such as those used in aircraft and stationary power generators, use large amounts of petroleum-based fuel and cause significant air pollution. The desire for energy independence and reduction in pollutant emissions has generated an interest in research on alternate fuels. Ethanol, which can also be derived from renewable energy sources, is an attractive alternate fuel. However, ethanol has a lower heating value than petroleum fuels. Hence, blending ethanol with petroleum fuels is a logical solution in the nearterm. Therefore, the effects of ethanol/Jet A blends on the performance and emission characteristics of a small-scale 30 kiloWatt gas turbine engine were studied. Blends of ethanol with Jet A in varying concentrations, ranging from 25 to 100% by volume, were used as fuels. The performance characteristics including the thrust, thrust-specific fuel consumption, and the emission properties, such as thrust-specific emission indices of CO and NOx, were measured for the different blends and compared with those obtained for Jet A over a range of throttle settings. The operational thrust range of the engine was reduced when compared to that available using Jet A fuel. The NOx emission was lower for the ethanol-Jet A blends because of lower temperature at the turbine inlet. The results indicate that n-ethanol-Jet A blend is a viable alternative fuel for gas turbine engines. Nomenclature EI i = emission index of a gas species (i) in the exhaust EI i, τ = thrust-specific emission index of a gas species in the exhaust f = fuel-to-air mass ratio m f = fuel flow rate MW fuel = molecular weight of fuel MW i = molecular weight of a gas species in the exhaust ρ f = fuel density ρ Jet A = density of Jet A fuel τ = static thrust x = average number of carbon atoms in fuel molecule X CO = mole fraction of carbon monoxide in exhaust X CO2 = mole fraction of carbon dioxide in exhaust X i = mole fraction of gas species (i) in the exhaust η th = thermal efficiency