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 abstract in SAE -- J v 66 n 7 July 1958 p 78-80)


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    Title :

    Turbine engines for high speed missiles


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1958 Propulsion



    Publication date :

    1958


    Size :

    15 pages


    Type of media :

    Conference paper


    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