Engine, developed by Bristol Aeroplane Co. has static thrust of 9750 lb and specific fuel consumption of 0.766 lb per lb of thrust per hr; compound axial flow engine designed for high speed long range applications. (See also Engineering v 174 n 4510 July 4 1952 p 13; Flight v 62 n 2267 July 4 1952 p 2-3; Aeroplane v 83 n 2137 July 4 1952 p 8-9)


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    Titel :

    "Olympus" turbojet engine


    Weitere Titelangaben:

    Engineer


    Erschienen in:

    Engineer ; 193 , n 5032


    Erscheinungsdatum :

    1952


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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