Type: Turbojet Thrust: 1,156 N (260 lb) at 34,000 rpm Compressor: 6-stage axial Combustor: Annular Turbine: Single-stage axial Weight: 63.5 kg (140 lb) Created by Doug Dammann Date Created 10/29/2021 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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