Type: Turbojet, afterburner Thrust: 133,440 N (30,000 lb) Compressor: 8-stage axial Combustor: Cannular Turbine: 2-stage Weight: 2,948 kg (6,500 lb) Created by Mark Avino Date Created 09/20/2017 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.