Advantages; description of straight turbojet engine and combined turbojet-ramjet engine for flight speeds in vicinity of Mach 4.0; performance at cruise conditions and in acceleration region presented for sample set of assumptions; typical missile applications. (See also Soc Automotive Engrs -- Paper n 48A for meeting Apr 8-11 1958 15 p)


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    Titel :

    Turbine engines for high speed missiles


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Neitzel, R.E. (Autor:in) / Zipkin, M.A. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Turbine engines for high speed missiles

    Neitzel, R.E. / Zipkin, M.A. | Engineering Index Backfile | 1958


    TURBINE ENGINES FOR HIGH SPEED MISSILES

    Zipkin, M. A. / NEITZEL, R. E. | SAE Technical Papers | 1958


    Turbine Engines for High-Speed Flight

    Henneberry, H. M. / Zimmerman, A. V. | NTRS | 1958


    Kinetic Heating of High Speed Missiles

    B. E. Richards | NTIS | 1979


    Gas-Turbine Engines of High-Speed Ships

    A. G. Kurzon / A. D. Mezheritskii / Y. I. Mityushkin et al. | NTIS | 1970