Type: Turbofan, two shaft Thrust: 3,740 N (840 lb st) class Fan: Approximate bypass ratio 1:1, 2-stage Compressor: 2 stage axial low-pressure, single stage centrifugal high-pressure Combustor: Folded annular Turbine: Single stage axial high-pressure, 2 stage low pressure Weight: 66 kg (145 lb) Created by Dane A. Penland Date Created 02/03/2014 Source Smithsonian National Air and Space Museum, National Air and Space Museum Original Photography, NASM Acc. 2012-0026 Keywords Aviation; Cold War; Engines; Jets; Propulsion Rights and Restrictions Usage conditions apply
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