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)
Bristol proteus
Aviation Week
Aviation Week ; 51 , n 17
1949
Article (Journal)
English
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Engineering Index Backfile | 1949
Online Contents | 2002
Engineering Index Backfile | 1951
Online Contents | 2001
Online Contents | 1994