Type: Turbojet, twin-spool Thrust: 44,480 N (10,000 lb) (dry) Compressor: 9-stage low-pressure axial; 7-stage high-pressure axial Combustor: 8 annular chambers Turbine: Three-stage axial Weight: 1,900 kg (4,200 lb) Created by Smithsonian National Air and Space Museum Date Created 11/01/2021 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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