Type: Turbojet Thrust: 4,657 N (1,047 lb) at 11,000 rpm Compressor: 8-stage axial Combustor: Annular Turbine: Single-stage axial Weight: 470 kg (1,035 lb) Created by Eric Long Date Created 11/15/2021 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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