THE Bristol Siddeley 75 turbofan, which has been designed primarily for civil applications, has a maximum sea level thrust of 7,550 lb. and is suitable for twin-engined short to medium range airliners of about 50,000 lb. all-up-weight, or four-engined airliners of 70,000 to 90,000 lb. all-up-weight.
Bristol Siddeley BS 75 Turbofan
Technical Features of the BS 75 Which Has a By-Pass Ratio of 1·75 to I
Aircraft Engineering and Aerospace Technology ; 34 , 7 ; 205
1962-07-01
1 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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