Type: Turbojet Thrust: 34,250 N (7,700 lb) at 8,300 rpm Compressor: 13-stage axial-flow compressor Combustor: Annular Turbine: 2-stage axial-flow Weight: 1,244 kg (2,742 lb) Created by Smithsonian National Air and Space Museum Date Created 05/02/2007 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Naval Aviation; People; Propulsion Rights and Restrictions Not determined
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