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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Turbine engines for high speed missiles


    Additional title:

    SAE -- J


    Contributors:


    Publication date :

    1958


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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