Type: Turbojet Thrust: 7,161 N (1,610 lb) at 16,500 rpm Compressor: Single-stage centrifugal Combustor: 10 reverse-flow combustion chambers Turbine: Single-stage axial Weight: 386 kg (850 lb) Created by Howard Wesoky Date Created 09/29/2005 Source Smithsonian National Air and Space Museum Keywords Aviation; Cold War; Engines; Jets; Propulsion Rights and Restrictions Not determined
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