THE Trident 2E is fitted with a further development of the Rolls-Royce Spey RB.163–25 turbofan engine, designated the Spey 25 Mk. 512–5W. This engine develops a nominal 12,000 lb. take-off thrust for a dry weight of 2,590 lb.


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    Title :

    Powerplant


    Subtitle :

    A brief description of the Spey 512 and RB.162 booster



    Publication date :

    1969-04-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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