Type: Turboshaft Power: 641 kw (860 hp) at 21,510 rpm Compressor: Five-stage axial, single-stage centrifugal Combustor: Reverse flow, 11 fuel nozzles Turbine: Single-stage axial gas generator, single-stage axial free power Created by Smithsonian National Air and Space Museum Date Created 09/29/2005 Source Smithsonian National Air and Space Museum Keywords Aviation; Engines; Jets; Propulsion Rights and Restrictions Not determined
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