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)
Bristol proteus
Engineering
Engineering ; 168 , n 4364
1949
3 pages
Article (Journal)
English
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Engineering Index Backfile | 1949
Engineering Index Backfile | 1949
Engineering Index Backfile | 1949
Development of "Bristol" Proteus propeller turbine engine
Engineering Index Backfile | 1954
|Bristol "Proteus III" (Series 700) propeller turbine
Engineering Index Backfile | 1952