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)
Chinook
Flight
Flight ; 53 , n 2039
1948
Article (Journal)
English
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