Type: Turbojet, 2-spool Thrust: 53,821 N (12,100 lb) at 8,200 rpm Compressor: 9-stage low pressure and 7-stage high pressure axial Combustor: 8 combustion chambers Turbine: Single-stage high pressure and 2-stage low pressure axial Weight (dry): 1,945 kg (4,285 lb) Created by Smithsonian National Air and Space Museum Date Created 10/12/2004 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
For more information, visit the Smithsonians Terms of Use.