Concord supersonic airliner, jointly produced by Sud Aviation and British Aircraft Corp, will be powered by Bristol Siddeley Olympus engines; these will be able to use existing aviation kerosene fuels for flight at speed of Mach 2.2; it probably may not be necessary to introduce thermal stability requirement into existing fuel specifications; since existing synthetic turbine engine lubricants are not quite good enough, some improvement is required, particularly in connection with thermal stability at high operating temperatures; description of 3 test rigs to evaluate gas turbine engine lubricants.


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    Title :

    Fuel and engine lubricant requirements for concord


    Additional title:

    SAE -- Paper


    Contributors:
    Morris, G. (author)

    Conference:

    SAE Meeting ; 1964



    Publication date :

    1964


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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