Kerosine-fueled turborocket offers advantages over rocket and turbojet engines for acceleration of recoverable space launcher to speeds of Mach 4-5 in short flight times; for particular flight plan examined, minimum power plant and fuel weight is 0.39 times aircraft takeoff weight, compared with 0.44 for turbojet and 0.58 for rocket; turborocket design is combination of turbojet and rocket; turborocket supplies up to 1/5 of total oxygen needed for combustion and operates by burning oxygen and fuel in rocket-type combustion chamber. Abbreviated version of paper presented at 1964 Annual Congress of Deutsche Gesellschaft fuer Raketentechnik u Raumfahrt (DGR).


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    Titel :

    Turborocket


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Lombard, A.A. (Autor:in) / Keenan, J.G. (Autor:in)

    Erschienen in:

    Flight ; 86 , n 2903


    Erscheinungsdatum :

    1964


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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