Type: Turbojet, single-shaft, Thrust: 4,412 N (992 lb) at 11,000 rpm Compressor: Single-stage, axial- flow inducer, centrifugal-flow Combustor: Gaseous annular reverse-flow Turbine: Single-stage radial Weight: 360 kg (794 lb) Created by Smithsonian National Air and Space Museum Date Created 02/07/2022 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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