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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    Titel :

    Fuel and engine lubricant requirements for concord


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Morris, G. (Autor:in)

    Kongress:

    SAE Meeting ; 1964



    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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