Why hypervelocity scramjets? - Airbreathing effective specific impulse (Isp) - Increase Two Stage to Orbit (TSTO) staging Mach number Hypervelocity challenges: - Many, in all disciplines (e.g. materials), primarily due to high enthalpy flow - Most challenging propulsion system: scramjet combustor (combustor residence time ~ 1 ms)


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    Titel :

    Hypervelocity Mixing Experiments at NASA Langley


    Beteiligte:
    Maxwell DePiro (Autor:in) / Tomasz Drozda (Autor:in) / Erik Axdahl (Autor:in) / Karen Cabell (Autor:in) / Paul Danehy (Autor:in)

    Kongress:

    NASA Fundamental Aeronautics Program 2012 Technical Conference ; 2012 ; Cleveland, OH, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






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