Type: Turbofan, dual spool Thrust: 436,000 N (98,000 lb) certified takeoff rating, 342,500 N (77,000 lb) maximum continuous rating Fan: Single stage, bypass ratio 5.8:1 Compressor: Six-stage axial low pressure, 11-stage axial high pressure Combustor: Annular, low NOx technology Turbine: Two-stage axial high pressure, 7-stage axial low pressure Weight: 7,264 kg (16,000 lb) Created by Smithsonian National Air and Space Museum Date Created 03/21/2022 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.