Engine, developed by Bristol Aeroplane Co. has static thrust of 9750 lb and specific fuel consumption of 0.766 lb per lb of thrust per hr; compound axial flow engine designed for high speed long range applications. (See also Engineering v 174 n 4510 July 4 1952 p 13; Flight v 62 n 2267 July 4 1952 p 2-3; Aeroplane v 83 n 2137 July 4 1952 p 8-9)
"Olympus" turbojet engine
Engineer
Engineer ; 193 , n 5032
1952
2 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1952
Engineering Index Backfile | 1952
Online Contents | 1996
Engineering Index Backfile | 1968
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