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

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


    Kinetic Heating of High Speed Missiles

    B. E. Richards | NTIS | 1979


    High Speed Pumps for Gas Turbine Engines

    Murray, J. F. | SAE Technical Papers | 1969


    Large rocket engines for space vehicles and missiles

    Hoffman, S.K. | Engineering Index Backfile | 1961