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; Aviation Week v 51 n 17 Oct 24 1949 p 21-2, 24-5, 27)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Bristol proteus


    Additional title:

    Engineering


    Published in:

    Engineering ; 168 , n 4364


    Publication date :

    1949


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Bristol proteus

    Engineering Index Backfile | 1949


    Bristol proteus

    Engineering Index Backfile | 1949


    Bristol proteus

    Engineering Index Backfile | 1949


    Development of "Bristol" Proteus propeller turbine engine

    Hooker, S.G. | Engineering Index Backfile | 1954