Type: Turbojet Thrust/Speed: 50,009 N (11,243 lb.) with afterburner (initial R-11 rating) Compressor: 6-stage low pressure and 3-stage high pressure Combustor: Can-annular, 10 flame tubes Turbine: Single-stage high pressure, single-stage low pressure axial Created by Smithsonian National Air and Space Museum Date Created 02/23/2022 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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