The Pegasus vectored-thrust turbofan is a 2-shaft design featuring three low pressure (LP) and eight high pressure (HP) compressor stages driven by two LP and two HP turbine stages respectively. The combustor is annular and features vaporisers. The latest variant, the 11-61, is controlled by a Full Authority Digital Engine Control (FADEC) system. The engine employs a simple thrust vectoring system that uses four swiveling nozzles, giving the Harrier thrust for both lift and forward propulsion.
| Rolls-Royce Holdings plc | |
|---|---|
| Product Category | Combustion Engines |
| Product Name | Pegasus Jet Engine |
| Fuel Type | Jet Fuel |
