Type: Turbofan Thrust: 97,900 N (22,000 lb) Fan: Bypass ratio 6:0, single-stage Compressor: 3-stage axial low pressure, 9-stage axial high pressure Combustor: Annular chamber Turbine: Single-stage axial high pressure, 4-stage axial low pressure Weight: 2,102 kg (4,635 lb) Created by Jim Preston Date Created 09/27/2022 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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