COMBUSTION CHAMBER INCLUDING INNER LINER FORMED WITH CERAMIC COMPOSITE MATERIAL, AND ITS METHOD FOR MANUFACTURE

摘要

PROBLEM TO BE SOLVED: To provide a combustion chamber which is capable of enduring a thermal load and various mechanical loads, and is useable for a rocket engine for example. SOLUTION: In the combustion chamber including at least one liner formed with a composite material involving a fiber texture comprising carbon containing fibers and a ceramic mother phase and being used for rocket engine for example, the fiber texture comprises a plurality of fiber layers 1a, 1b, and 1c, and the plurality of the fiber layers form a three dimensional structure.