• Pratt & Whitney JSF119-PW-611C Turbofan Engine
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    Type: Turbofan, Twin-Spool, Augmented Thrust: 186.9 kN (42,000 lb) Total Vertical Lift Thrust: 164.6 kN (37,000 lb) Fan: Bypass ratio 0.45, 3-stage Compressor: 6 stage axial Combustor: Annular Turbine: Single stage axial high-pressure, single stage axial low pressure Weight: 1,771 kg (3,900 lb)

Created by

Dane Penland

Date Created

11/12/2010

Source

Smithsonian National Air and Space Museum

Keywords

Aviation; Engines; Jets; Propulsion

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