Turbo Research, Ltd, started design of Chinook and work was completed at Avro Canada plant at Malton; information will be used for more powerful units already on design boards or in component manufacturing stage; max design power is 2500 lb thrust at 10,000 rpm and unit has 9-stage axial flow compressor, six combustion chambers and single stage turbine; max diam 32 in.; oa length 125 in.; total weight 1250 lb. (See also Aero Digest v 57 n 3 Sept 1948 p 106-7)


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    Title :

    Chinook


    Additional title:

    Flight


    Published in:

    Flight ; 53 , n 2039


    Publication date :

    1948


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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