A Mach 10 cruise vehicle provides a quick response, global reach capability with high survivability. For operations from CONUS, mission radii on the order of 8,000 nmi are sufficient. For missions which return to CONUS, a dual-fueled vehicle is superior, due to its capability to in-flight refuel. However, for one-way mission, an all-hydrogen vehicle is preferable because of its higher specific impulse.


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    Titel :

    NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study


    Beteiligte:

    Erscheinungsdatum :

    01.01.1996


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Hunt, James / Eiswirth, Edward | AIAA | 1996


    NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study

    J. L. Hunt / E. A. Eiswirth | NTIS | 2005


    NASA Dual Fuel Airbreathing Hypersonic Vehicle Study

    Hunt, J. / Eiswirth, E. / AIAA | British Library Conference Proceedings | 1996