Eads Space Transportation Gmbh

Peter Bichler

Steffen Beyer

Dieter Kunzmann

Wolfgang Keinath

Roland Kindermann

A combustion chamber structure for a rocket engine or the like, has a combustion chamber liner with cooling channels and at least one manifold for feeding and removing a coolant, particularly a cryogenic fuel. The at least one manifold is brazed together with the combustion chamber liner and the area of the combustion chamber liner that is not covered by the at least one manifold is coated with an electroplated structural jacket. The invention also includes a method for manufacturing the combustion chamber structure.

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Munich, Georgia

Peter Bichler