Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung

摘要

A structural part for use as a wall of a device subject to high temperatures, such as rocket combustion chamber, heat shield, nose cone of a missile etc., includes individual tubular form elements having either an opened or a closed cross section which are fitted together to form a wall and which are connected mechanically strong and pressure proof by a layer of material which is electroformed on either one or both sides thereof. Various structural configurations are possible and in some instances the resultant structure is reinforced by a reinforcing member such as a steel strip.