A method for start-up of a gas turbine engine powered by combusting a hydrocarbonaceous fuel in an oxygen-containing gas mixture, said gas turbine engine employing a monolithic, electrically-heated catalyst structure being comprised of heat resistant, thin metal foils, at least one of which is corrugated, and said foils being stacked together to form a plurality of adjacent longitudinal channels for passage of said fuel and oxygen-containing gas mixture wherein at least a portion of the channels is coated with a catalyst and the interior surface of the remaining channels is not coated with catalyst and at least some portions of the foils are coated with an electrically-insulative coating on at least one side, said foils being connected to electrode and to each other to form an electrical circuit whereby, upon application of electrical power having a predetermined voltage, a current will flow through some portion of the metal foils thereby heating said foils, said method comprising the steps of:
- a. applying electrical power to said catalyst structure to heat said catalyst structure to within about 100.degree. C. of the steady-state operating temperature of said catalyst structure;
- b. contacting said preheated catalyst structure with said hydrocarbonaceous fuel/oxygen-containing gas mixture;
- and
- c. terminating said electrical power when any one of the following predetermined condition are met:
- i. the heat of reaction released by the reaction of the fuel and oxygen on said catalyst structure is sufficient to maintain said catalyst structure at its steady-state operating temperature, or
- ii. the fuel/oxygen-containing mixture at the combustor outlet reaches a predetermined temperature limit,
- iii. a predetermined period of time has elapsed since said contacting step was initiated, or
- iv. the partially combusted fuel oxygen-containing mixture at the catalyst exit reaches a predetermined temperature.