Bristol Siddeley BS 75 Turbofan

Name: Bristol Siddeley BS 75 Turbofan
Keywords: 7. Clean energy

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Aircraft Engineering and Aerospace Technology

Article . 1962 . Peer-reviewed

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Bristol Siddeley BS 75 Turbofan

Technical Features of the BS 75 Which Has a By‐Pass Ratio of 1·75 to I

descriptionPublicationkeyboard_double_arrow_right Article 01 Jul 1962 English Publisher:EmeraldJournal:Aircraft Engineering and Aerospace Technology, volume 34, pages 205-205 (issn: 0002-2667,

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doi: 10.1108/eb033578

Bristol Siddeley BS 75 Turbofan

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Abstract

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.

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