THE AEROTHERMAL, THERMAL AND STRUCTURAL DESIGN PROCESS AND CRITERIA FOR THE HIFIRE-4 FLIGHT TEST VEHICLE
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
2012-01-01
17 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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