Type: Turbofan Thrust: 19,224 N (4,320 lb) at 19,280 rpm Fan: Bypass ratio 6:1, single stage Compressor: Single-stage fan, 7-stage axial, 1-stage centrifugal Combustor: Annular reverse flow Turbine: Single-stage core, 2-stage free power turbine driving fan Weight: 374 kg (825 lb) Created by Smithsonian National Air and Space Museum Date Created 09/29/2005 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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