Type: Turbojet Thrust: 7,118 N (1,600 lb) at 16,500 rpm Compressor: Single-stage centrifugal Combustor: 10 reverse flow chambers Turbine: Single-stage axial Weight: 386 kg (850 lb) Created by Jonathan R. Barrett Date Created 09/16/2014 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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