• Metal engine displayed in an exhibit case with exposed components: intake, compressor, combustion chamber, and exhaust. The engine fan has a gray and black cone with a white pattern on the tip.
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    Type: Turbofan Thrust: 97,900 N (22,000 lb) Fan: Bypass ratio 6:0, single-stage Compressor: 3-stage axial low pressure, 9-stage axial high pressure Combustor: Annular chamber Turbine: Single-stage axial high pressure, 4-stage axial low pressure Weight: 2,102 kg (4,635 lb)

Created by

Jim Preston

Date Created

09/27/2022

Source

Smithsonian National Air and Space Museum

Keywords

Aviation; Engines; Jets; Propulsion

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