Multi-Disciplinary Design of a Rocket Engine Thrust Augmentation Ejector for Endoatmospheric Flight (AIAA 2014-3091)
19th, AIAA international space planes and hypersonic systems and technologies conference ; 2014 ; Atlanta, GA
01.01.2014
21 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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Near-Field Acoustical Characterization of Clustered Rocket Engines AIAA Paper 2005-3091
British Library Conference Proceedings | 2005
|AIAA | 2010
|Online Contents | 2010
|Compact Ejector Thrust Augmentation
AIAA | 1973
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