• Bristol-Siddeley Pegasus Mk. 5 Turbofan Engine
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    Type: Turbofan, vectored thrust VTOL engine, 4 swivel exhausts Thrust: 68,944 N (15,500 lb) at take-off Compressor: 2-stage front fan, bypass; 7-stage axial Combustor: Cannular Turbine: 3-stage axial Weight: 975 kg (2,150 lb)

Created by

Dane Penland

Date Created

08/19/2014

Source

Smithsonian National Air and Space Museum, NASM Original Photography, NASM Acc. 2012-0026.

Keywords

Aviation; Cold War; Engines; Jets; Propulsion

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