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Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The dual-bell rocket nozzle was first proposed in 1949, offering a potential improvement in rocket nozzle performance over the conventional-bell nozzle. Despite the performance advantages that have been predicted, both analytically and through static