| Tumansky RD-9 ✕ | ALF 502R-3 ✕ | |
|---|---|---|
| EASA ID | 1TL002 | |
| Aircraft Engine Manufacturer | Shenyang | Textron Lycoming |
| 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 | |
| Geared Fan | No | Yes |
| Afterburner | Yes | No |
| Streams | 1 | 2 |
| Bypass Ratio | 5.7 | |
| Overall Pressure Ratio | 11.4 | |
| Maximum Takeoff Thrust (kN) | 29 | 29.8 |
| Thrust To Weight | 5.2 | |
| Hydrocarbon Take Off (g/kg fuel) | 0.056 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0.053 | |
| Hydrocarbon Approach (g/kg fuel) | 0.287 | |
| Hydrocarbon Idle (g/kg fuel) | 6.51 | |
| Hydrocarbon Unitary Average (g/kN) | 15 | |
| Hydrocarbon Unitary Sigma (g/kN) | 3.25 | |
| Hydrocarbon Unitary Range (g/kN) | 11.9-18.4 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 17.5 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 89.3 | |
| Hydrocarbon LTO (g) | 449 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0.433 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.5 | |
| Carbon Monoxide Approach (g/kg fuel) | 8.43 | |
| Carbon Monoxide Idle (g/kg fuel) | 44.67 | |
| Carbon Monoxide Unitary Average (g/kN) | 109 | |
| Carbon Monoxide Unitary SD (g/kN) | 10.62 | |
| Carbon Monoxide Unitary Range (g/kN) | 100.2-120.8 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 117.9 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 99.9 | |
| NOx Take Off (g/kg fuel) | 11.2 | |
| NOx Climb Out (g/kg fuel) | 9.94 | |
| NOx Approach (g/kg fuel) | 6.15 | |
| NOx Idle (g/kg fuel) | 3.3 | |
| NOx Unitary Average (g/kN) | 30.7 | |
| NOx Unitary SD (g/kN) | 0.795 | |
| NOx Unitary Range (g/kN) | 29.9-31.45 | |
| NOx Unitary Characteristic (g/kN) | 32.5 | |
| NOx Unitaryto Standard (% of limit) | 51.8 | |
| NOx Unitaryto CAEP2 (% of limit) | 64.7 | |
| NOx Unitaryto CAEP4 (% of limit) | 65.5 | |
| NOx Unitaryto CAEP6 (% of limit) | 65.8 | |
| NOx Unitaryto CAEP8 (% of limit) | 69.8 | |
| NOx LTO (g) | 915 | |
| Smoke Take Off (SN) | 12.63 | |
| Smoke Climb Out (SN) | 12 | |
| Smoke Approach (SN) | 5.47 | |
| Smoke Idle (SN) | 2.133 | |
| Smoke Max (SN) | 13 | |
| Smoke Sigma (SN) | 2.39 | |
| Smoke Range (SN) | 10.2-14.4 | |
| Smoke Characteristic (SN) | 14.3 | |
| Smoke Characteristicto Regulatory (% of limit) | 43.4 | |
| Fuel Flow Take Off (kg/s) | 0.3476 | |
| Fuel Flow Climbout (kg/s) | 0.288 | |
| Fuel Flow Approach (kg/s) | 0.1027 | |
| Fuel Flow Idle (kg/s) | 0.0432 | |
| Fuel LTO (kg) | 145 | |
| Fuel Venting Compliant | No | |
| Afterburner Thrust (kN) | 37 | |
| Carbon Monoxide LTO (g) | 3244 | |
| Compressor Description | Single-spool 9-stage Axial compressor | |
| Emissions Data Status | C | |
| Engine Status | Out of production | |
| Turbine Description | axial flow |