AS is to be expected, the various systems on the Trident 2E closely follow those evolved for the Tridents 1 and 1E, except for the changes in the fuel system necessitated by the introduction of the fin fuel tank, and the embodiment of a turbine-compressor type of cold air unit in the air conditioning system.


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    Title :

    Trident 2E Aircraft Systems


    Subtitle :

    Details of fuel system, electrical power installation, hydraulic system, air conditioning and pressurisation and flying controls



    Publication date :

    1969-04-01


    Size :

    11 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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