Abstract:A research airplane was studied which has potential for large-scale demonstration of advanced propulsive, structural, and aerodynamic technologies for hypersonic application. Versatility is achieved through the selection of a configuration that provides for scramjet engine integration by the extensive performance envelope and by large removable sections of the airplane. After a screening of alternative structural concepts, design criteria were applied to an effective heat-sink structure of Lockalloy (Be-38 AI)… Show more
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