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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    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






    NASA Langley Transformation Plan

    Cara A C Leckey / H Kevin Rivers | NTRS | 2023