Illustrated design analysis of high compression turboprop for wing mounting; length 113.35 in.; oa diam 38.5 in.; weight (bare) 2900 lb; output (35,000 ft, 350 mph) 1260 shp plus 560 lb thrust. (See also Flight v 56 n 2121 Aug 18 1949 p 191-6; Engineer v 188 n 4884 Sept 2 1949 p 260-2; Engineering v 168 n 4364 Sept 16 1949 p 269-71)


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    Title :

    Bristol proteus


    Additional title:

    Aviation Week


    Published in:

    Aviation Week ; 51 , n 17


    Publication date :

    1949


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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