AIAA-2005-1025 SCRAMJET ENGINE FLOWPATH DEVELOPMENT FOR THE HYPER-X MACH 10 FLIGHT TEST
17th, International symposium on air breathing engines ; 2005 ; Munich, Germany
2005-01-01
17 pages
Includes bibliographical references and index; Papers on CD-ROM
Aufsatz (Konferenz)
Englisch
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AIAA | 2001
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