Type: Turbojet, single-shaft Thrust: 12,680 N (2,850lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 181 kg (398 lb) Created by Eric Long Date Created 06/09/2016 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Usage conditions apply
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