Four regenerator matrix samples, fabricated by different manufacturing methods and consisting of different ceramic materials and cell geometries, were studied to determine their reliability and performance potential in a typical industrial gas turbine engine. Hypothetical regenerators were designed from these matrix samples to give identical engine performance, and the thermal stress was determined for each. In some instances, it was necessary to stress relieve and preload the rims in order to reduce the thermal stresses so that acceptable reliability could be obtained. The four hypothetical regenerators were then compared on the basis of size, cost, leakage, etc., so that the advantages of each configuration could be observed.The performance and reliability analysis was based on Ford Motor Company's shuttle rig performance tests and over 200,000 core-hours of engine test on ceramic regenerators. The engine test program is described in detail.