The RB199 is a 3-shaft reheated turbofan engine, with three low pressure (LP), three intermediate pressure (IP) and six high pressure (HP) compressor stages, powered by two single-stage turbines (HP and IP) and a 2-stage LP turbine. The combustion system is of annular vaporising design. Engine control is by a Full Authority Digital Engine Control (FADEC) system and features an integral thrust reverser
| Rolls-Royce Holdings plc | |
|---|---|
| Product Category | Combustion Engines |
| Product Name | RB199 Jet Engine |
| Fuel Type | Jet Fuel |
