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View article: Dual-Bell Nozzle Design
Dual-Bell Nozzle Design Open
The dual-bell nozzle is an altitude adaptive nozzle concept that offers two operation modes. In the framework of the German Research Foundation Special Research Field SFB TRR40, the last twelve years have been dedicated to study the dual-b…
View article: CNES/DLR cooperation for the preparation of future reusable launcher cryogenic engines
CNES/DLR cooperation for the preparation of future reusable launcher cryogenic engines Open
Cooperation has started between the German Aerospace Centre, DLR Lampoldshausen and the launcher directorate of the French National Centre for Space studies CNES. Aim of the collaboration is the preparation of technologies and tools for th…
View article: Parametrical study on side load generation in subscale rocket nozzles
Parametrical study on side load generation in subscale rocket nozzles Open
The flow separation within convergent–divergent rocket engine nozzles induces undesired side loads. As the flow separation cannot be avoided during startup and shutdown processes of the engine, the understanding of the resulting side loads…
View article: Rocket Propulsion in TAU: An Overview of the DLR ProTAU Project
Rocket Propulsion in TAU: An Overview of the DLR ProTAU Project Open
The ProTAU project is an internal cooperation between several DLR institutes to advance the independent DLR expertise in modelling rocket propulsion systems and their components. The focus is on the development and validation of the DLR in…