| Tumansky RD-9 ✕ | AE3007C ✕ | |
|---|---|---|
| EASA ID | 3AL001 | |
| Aircraft Engine Manufacturer | Shenyang | Rolls-Royce |
| Aircraft Engine Type | Turbojet | Turbofan |
| Dry Weight (kg) | 725 | |
| Diameter (mm) | 668 | |
| Length (mm) | 5560 | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Tumansky_RD-9 | |
| Fuel | Jet A/JP-8 | |
| Geared Fan | No | No |
| Afterburner | Yes | No |
| Streams | 1 | 2 |
| Bypass Ratio | 5.3 | |
| Overall Pressure Ratio | 16.2 | |
| Maximum Takeoff Thrust (kN) | 29 | 28.6 |
| Thrust To Weight | 5.2 | |
| Hydrocarbon Take Off (g/kg fuel) | 0.29 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0.33 | |
| Hydrocarbon Approach (g/kg fuel) | 0.83 | |
| Hydrocarbon Idle (g/kg fuel) | 5.84 | |
| Hydrocarbon Unitary Average (g/kN) | 13.46 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 17.5 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 89.3 | |
| Hydrocarbon LTO (g) | 387 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0.97 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 1.19 | |
| Carbon Monoxide Approach (g/kg fuel) | 4.5 | |
| Carbon Monoxide Idle (g/kg fuel) | 29.88 | |
| Carbon Monoxide Unitary Average (g/kN) | 68 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 77.5 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 65.7 | |
| NOx Take Off (g/kg fuel) | 16.92 | |
| NOx Climb Out (g/kg fuel) | 14.56 | |
| NOx Approach (g/kg fuel) | 6.63 | |
| NOx Idle (g/kg fuel) | 3.24 | |
| NOx Unitary Average (g/kN) | 34.73 | |
| NOx Unitary Characteristic (g/kN) | 38.2 | |
| NOx Unitaryto Standard (% of limit) | 52.8 | |
| NOx Unitaryto CAEP2 (% of limit) | 66 | |
| NOx Unitaryto CAEP4 (% of limit) | 66.4 | |
| NOx Unitaryto CAEP6 (% of limit) | 66.6 | |
| NOx Unitaryto CAEP8 (% of limit) | 70.4 | |
| NOx LTO (g) | 991 | |
| Smoke Take Off (SN) | 1 | |
| Smoke Climb Out (SN) | 0 | |
| Smoke Approach (SN) | 0 | |
| Smoke Idle (SN) | 0 | |
| Smoke Max (SN) | 1 | |
| Smoke Characteristic (SN) | 1.2 | |
| Smoke Characteristicto Regulatory (% of limit) | 3.6 | |
| Fuel Flow Take Off (kg/s) | 0.28 | |
| Fuel Flow Climbout (kg/s) | 0.234 | |
| Fuel Flow Approach (kg/s) | 0.091 | |
| Fuel Flow Idle (kg/s) | 0.039 | |
| Fuel LTO (kg) | 125 | |
| Fuel Venting Compliant | No | |
| Afterburner Thrust (kN) | 37 | |
| Carbon Monoxide LTO (g) | 1964 | |
| Compressor Description | Single-spool 9-stage Axial compressor | |
| Emissions Data Status | C | |
| Emissions Data Superseded | Yes | |
| Emissions Superseded By | 6AL021 | |
| Engine Status | Out of production | |
| Turbine Description | axial flow |