| TAY 650 ✕ | Lyulka AL-7 ✕ | |
|---|---|---|
| EASA ID | 3RR031 | |
| Aircraft Engine Manufacturer | Rolls-Royce | Lyulka-Saturn |
| Aircraft Engine Type | Turbofan | Turbojet |
| Dry Weight (kg) | 2010 | |
| Diameter (mm) | 1300 | |
| Length (mm) | 6650 | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Lyulka_AL-7 | |
| Fuel | AVTUR | |
| Geared Fan | No | No |
| Combustion Chamber | Pedhead | Annular |
| Afterburner | No | Yes |
| Streams | 2 | 1 |
| Bypass Ratio | 3 | |
| Overall Pressure Ratio | 15.9 | |
| Maximum Takeoff Thrust (kN) | 67.2 | 67.1 |
| Thrust To Weight | 3.4 | |
| Hydrocarbon Take Off (g/kg fuel) | 0.11 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0.22 | |
| Hydrocarbon Approach (g/kg fuel) | 0.11 | |
| Hydrocarbon Idle (g/kg fuel) | 1.23 | |
| Hydrocarbon Unitary Average (g/kN) | 3.9 | |
| Hydrocarbon Unitary Range (g/kN) | 3.9 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 6 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 30.6 | |
| Hydrocarbon LTO (g) | 261 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0.69 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.48 | |
| Carbon Monoxide Approach (g/kg fuel) | 1.76 | |
| Carbon Monoxide Idle (g/kg fuel) | 22.36 | |
| Carbon Monoxide Unitary Average (g/kN) | 65.16 | |
| Carbon Monoxide Unitary Range (g/kN) | 62.4-67.9 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 80 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 67.8 | |
| NOx Take Off (g/kg fuel) | 16.45 | |
| NOx Climb Out (g/kg fuel) | 12.94 | |
| NOx Approach (g/kg fuel) | 5.26 | |
| NOx Idle (g/kg fuel) | 2.5 | |
| NOx Unitary Average (g/kN) | 38.75 | |
| NOx Unitary Range (g/kN) | 38.1-39.5 | |
| NOx Unitary Characteristic (g/kN) | 44.9 | |
| NOx Unitaryto Standard (% of limit) | 62.6 | |
| NOx Unitaryto CAEP2 (% of limit) | 78.2 | |
| NOx Unitaryto CAEP4 (% of limit) | 91.6 | |
| NOx Unitaryto CAEP6 (% of limit) | 98.7 | |
| NOx Unitaryto CAEP8 (% of limit) | 115.8 | |
| NOx LTO (g) | 2591 | |
| Smoke Take Off (SN) | 5.6 | |
| Smoke Climb Out (SN) | 7.9 | |
| Smoke Approach (SN) | 4 | |
| Smoke Idle (SN) | 0.56 | |
| Smoke Max (SN) | 9.87 | |
| Smoke Range (SN) | 9.3-10.4 | |
| Smoke Characteristic (SN) | 12.7 | |
| Smoke Characteristicto Regulatory (% of limit) | 48.1 | |
| Fuel Flow Take Off (kg/s) | 0.86 | |
| Fuel Flow Climbout (kg/s) | 0.71 | |
| Fuel Flow Approach (kg/s) | 0.25 | |
| Fuel Flow Idle (kg/s) | 0.12 | |
| Fuel LTO (kg) | 377 | |
| Fuel Venting Compliant | No | |
| Carbon Monoxide LTO (g) | 4361 | |
| Compressor Description | Single-spool turbojet 9-stage axial compressor | |
| Emissions Data Status | C | |
| Engine Status | Out of production | |
| Turbine Description | 2-stage axial |