Type: Turbojet Thrust: 6,894 N (1,550 lb) at 9,000 rpm Compressor: 7-stage axial Combustor: Annular Turbine: Single-stage axial Weight: 624 kg (1,375 lb.) Created by Dane A. Penland Date Created 06/26/2014 Source Smithsonian National Air and Space Museum, , NASM Acc. 2012-0026 Keywords Aviation; Engines; Jets; Propulsion; World War II Rights and Restrictions Usage conditions apply
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