Type: Turbojet Thrust: 4,561 N (1,025 lb thrust) at 21,730 rpm Compressor: Single-stage centrifugal Combustor: Annular Turbine: Single-stage axial Weight: 165 kg (364 lb) Created by Eric Long Date Created 11/17/2021 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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