Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb) Created by Jason A. Smith Date Created 07/28/2017 Source National Air and Space Museum, Smithsonian Institution. Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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