Hyper-X Mach 10 engine flowpath development - Fifth entry test conditions and methodology
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference ; 2001 ; Kyoto , Japan
01.01.2001
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2005-1025 SCRAMJET ENGINE FLOWPATH DEVELOPMENT FOR THE HYPER-X MACH 10 FLIGHT TEST
British Library Conference Proceedings | 2005
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