Raketentriebwerk in Segmentbauweise

摘要

The invention relates to a method for producing a rocket drive and to a rocket drive which has a combustion chamber (1) and an expansion nozzle (2) which adjoins the combustion chamber (1). At least two single-piece segment bodies (4a, 4b, 4c) are provided, each segment body (4a, 4b, 4c) forming partial contours of the combustion chamber (1) and the expansion nozzle (2). Said segment bodies are brought together in order to form the combustion chamber (1) and the expansion nozzle (2).