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 Engineer v 188 n 4884 Sept 2 1949 p 260-2; Engineering v 168 n 4364 Sept 16 1949 p 269-71; Aviation Week v 51 n 17 Oct 24 1949 p 21-2, 24-5, 27)


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    Title :

    Bristol proteus


    Additional title:

    Flight


    Published in:

    Flight ; 56 , n 2121


    Publication date :

    1949


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Bristol proteus

    Engineering Index Backfile | 1949


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    Engineering Index Backfile | 1949


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