Type: Turbojet, afterburner Thrust: 66,7000 N (15,000 lb) Compressor: 17-stage axial Combustor: Cannular Turbine: 3-stage axial Weight (dry): 1,642 kg (3,620 lb) Created by Eric Long Date Created 03/24/2011 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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