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
2014-01-01
21 pages
Includes bibliographical references and author index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA | 2010
|Near-Field Acoustical Characterization of Clustered Rocket Engines AIAA Paper 2005-3091
British Library Conference Proceedings | 2005
|Online Contents | 2010
|AIAA | 1992
|