Combustion chamber apparatus for rocket engine, has casing with sections of wall of combustion chamber and forming wall of nozzle extension, and injection head that extends to opposite end of nozzle extension

摘要

The combustion chamber apparatus (100) comprises a combustion chamber (106), an injection head (104) for feeding one fluid to the combustion chamber, and a nozzle extension (108). A casing (148) comprises sections of a wall (146) of the combustion chamber and forms a wall (150) of the nozzle extension. The injection head extends to the opposite end of the nozzle extension, in the device assembled state. An independent claim is included for method for manufacturing the combustion chamber apparatus.