Type: Turbojet Thrust/speed: 8,807 N (1,980 lb) at 8,700 rpm Compressor: 8-stage axial Combustor: 6 straight-through chambers Turbine: Single-stage axial Manufacturer: Junkers Flugzeug und Motorenwerke A.G., Dessau, Germany Created by Mark Avino Date Created 05/19/2016 Source Smithsonian National Air and Space Museum. Keywords Aviation; Engines; Jets; Propulsion; Records & Firsts Rights and Restrictions Usage conditions apply
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