Type: Turboshaft Power Rating: 224 kW (300 hp) at 28,380 rpm Compressor: Single-stage centrifugal Combustor: 2 combustion chambers Turbine: Single-stage axial Weight: 152 kg (334 lb) Created by Dane A. Penland Date Created 02/03/2014 Source Smithsonian National Air and Space Museum, National Air and Space Museum Original Photography, NASM Acc. 2012-0026 Keywords Aviation; Cold War; Engines; Jets; Propulsion Rights and Restrictions CC0
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