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)
Bristol proteus
Flight
Flight ; 56 , n 2121
1949
6 pages
Aufsatz (Zeitschrift)
Englisch
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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