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; Engineer v 193 n 5032 July 4 1952 p 24-5; Aeroplane v 83 n 2137 July 4 1952 p 8-9)
"Olympus" turbojet engine
Flight
Flight ; 62 , n 2267
1952
2 pages
Article (Journal)
English
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