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; Engineer v 193 n 5032 July 4 1952 p 24-5; Aeroplane v 83 n 2137 July 4 1952 p 8-9)


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    Title :

    "Olympus" turbojet engine


    Additional title:

    Flight


    Published in:

    Flight ; 62 , n 2267


    Publication date :

    1952


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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