Rocket combustion chamber.

摘要

The chamber is formed by a first section comprising the body (14) and the jet pipe neck (18) and a second section comprising the jet pipe diffuser nozzle (22) extended upstream by a wall (24) surrounding the first section and providing a clearance with it. The connection between the first and second sections is made in an area located on a level with or close to the upstream end of the chamber connected to the ergols injector (30). <IMAGE>