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Showing 1 to 2 of 2 for “"Raketentriebwerk"”.
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Systemanalytische Untersuchung einer Brennkammer in faserkeramischer Bauweise von Raketenantrieben
This work describes an analytic model for evaluation of expected effects of the use of ceramic materials in the construction of rocket engine thrust chambers. An engine of a thrust level around 1500 kN is defined and analyzed. The engine analysis makes use of the DLR tool LRP, which calculates …
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Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer
The goal of this thesis is to determine the influence of different phenomena on the heat load of a hydrogen/oxygen rocket combustion chamber into the adjacent regenerative cooled wall. The heat transfer in turbulent flow is a result of turbulent vortices and the heat conductivity of the fluid. The …