THE Bristol Siddeley 75 turbofan, which has been designed primarily for civil applications, has a maximum sea level thrust of 7,550 lb. and is suitable for twin-engined short to medium range airliners of about 50,000 lb. all-up-weight, or four-engined airliners of 70,000 to 90,000 lb. all-up-weight.


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    Titel :

    Bristol Siddeley BS 75 Turbofan


    Untertitel :

    Technical Features of the BS 75 Which Has a By-Pass Ratio of 1·75 to I



    Erscheinungsdatum :

    1962-07-01


    Format / Umfang :

    1 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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