Type: Turbofan, two-shaft, geared Thrust/speed: 16,500 N (3,700 lb) at 29,692 rpm Fan: Bypass ratio 2.8:1, single-stage, Compressor: 4-stage low-pressure axial, 1-stage high-pressure centrifugal Combustor: Annular reverse flow Turbine: Single-stage high-pressure, 3-stage low-pressure Weight: 342 kg (754 lb) Created by Jim Preston Date Created 09/21/2022 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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