Type: Turbojet Thrust: 5,516 N (1,240 lb) at 17,750 rpm, 3,781 N (850 lb) at 16,500 rpm (Derated for first flight) Compressor: Single-stage, double entry, centrifugal Combustor: 10 reverse flow chambers Turbine: Single- stage axial Weight: 254 kg (560 lb) Created by Dane Penland Date Created 02/11/2016 Source Smithsonian National Air and Space Museum, NASM Original Photography, NASM Acc. 2012-0026. Keywords Aviation; Engines; Jets; Propulsion; Records & Firsts; World War II Rights and Restrictions CC0
For more information, visit the Smithsonians Terms of Use.