Comparative Flowpath Analysis and Design Assessment of a Mach 6.5 Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine
International conference; 7th, Space planes and hypersonic systems and technologies ; 1996 ; Norfolk; VA
1996-01-01
AIAA-96-4571
Paper nos 4490-4596. Also known as the 7th International aerospace plane and hypersonic technologies conference and also the 7th International spaceplanes and hypersonics systems and technology conference
Conference paper
English
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AIAA-2005-1025 SCRAMJET ENGINE FLOWPATH DEVELOPMENT FOR THE HYPER-X MACH 10 FLIGHT TEST
British Library Conference Proceedings | 2005
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