Feasibility study of several new proposed propulsion concepts for sustained hypersonic propulsion using terrestrial atmosphere; processes are evaluated in light of their energy production and flight energy requirements; energy released by stationary and moving detonation waves is computed and compared with propulsion requirements; proposed hypersonic airbreathing propulsion system applications, including electrical augmentation, are evaluated; electromagnetic fuel injection afterburner combined with fuel-lean standing wave detonation process appears most promising; exploratory experiments.


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    Titel :

    Terrestrial hypersonic flight propulsion


    Weitere Titelangaben:

    AIAA-ASME -- Paper


    Beteiligte:
    Foreman, K.M. (Autor:in)

    Kongress:

    AIAA-ASME Hypersonic Ramjet Conference ; 1963 Afterburners


    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch







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