| Tumansky RD-9 ✕ | PW307A ✕ | |
|---|---|---|
| EASA ID | 16PW114 | |
| Aircraft Engine Manufacturer | Shenyang | Pratt & Whitney Canada |
| 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-1 | |
| Geared Fan | No | No |
| Combustion Chamber | TALON II | |
| Afterburner | Yes | No |
| Streams | 1 | 2 |
| Bypass Ratio | 4.2 | |
| Overall Pressure Ratio | 20.21 | |
| Maximum Takeoff Thrust (kN) | 29 | 28.49 |
| Thrust To Weight | 5.2 | |
| Hydrocarbon Take Off (g/kg fuel) | 0 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0 | |
| Hydrocarbon Approach (g/kg fuel) | 0 | |
| Hydrocarbon Idle (g/kg fuel) | 1.99 | |
| Hydrocarbon Unitary Average (g/kN) | 4.8 | |
| Hydrocarbon Unitary Sigma (g/kN) | 1.5 | |
| Hydrocarbon Unitary Range (g/kN) | 3.2-6.2 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 5.6 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 28.6 | |
| Hydrocarbon LTO (g) | 137 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0.27 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.23 | |
| Carbon Monoxide Approach (g/kg fuel) | 3.23 | |
| Carbon Monoxide Idle (g/kg fuel) | 36.92 | |
| Carbon Monoxide Unitary Average (g/kN) | 91.6 | |
| Carbon Monoxide Unitary SD (g/kN) | 6.5 | |
| Carbon Monoxide Unitary Range (g/kN) | 85.4-98.4 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 99.1 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 84 | |
| NOx Take Off (g/kg fuel) | 18.28 | |
| NOx Climb Out (g/kg fuel) | 15.58 | |
| NOx Approach (g/kg fuel) | 8.77 | |
| NOx Idle (g/kg fuel) | 2.86 | |
| NOx Unitary Average (g/kN) | 42.8 | |
| NOx Unitary SD (g/kN) | 0.7 | |
| NOx Unitary Range (g/kN) | 42-43.3 | |
| NOx Unitary Characteristic (g/kN) | 45.3 | |
| NOx Unitaryto Standard (% of limit) | 56.3 | |
| NOx Unitaryto CAEP2 (% of limit) | 70.4 | |
| NOx Unitaryto CAEP4 (% of limit) | 70.8 | |
| NOx Unitaryto CAEP6 (% of limit) | 71 | |
| NOx Unitaryto CAEP8 (% of limit) | 75 | |
| NOx LTO (g) | 1221 | |
| Smoke Take Off (SN) | 0.65 | |
| Smoke Climb Out (SN) | 0.32 | |
| Smoke Approach (SN) | 0 | |
| Smoke Idle (SN) | 1.69 | |
| Smoke Max (SN) | 1.7 | |
| Smoke Sigma (SN) | 0.2 | |
| Smoke Range (SN) | 1.5-1.9 | |
| Smoke Characteristic (SN) | 1.9 | |
| Smoke Characteristicto Regulatory (% of limit) | 5.7 | |
| Fuel Flow Take Off (kg/s) | 0.327 | |
| Fuel Flow Climbout (kg/s) | 0.272 | |
| Fuel Flow Approach (kg/s) | 0.102 | |
| Fuel Flow Idle (kg/s) | 0.044 | |
| Fuel LTO (kg) | 143 | |
| Fuel Venting Compliant | Yes | |
| Afterburner Thrust (kN) | 37 | |
| Carbon Monoxide LTO (g) | 2625 | |
| Compressor Description | Single-spool 9-stage Axial compressor | |
| Emissions Data Status | C/R | |
| Emissions Data Superseded | Yes | |
| Emissions Superseded By | 01P16PW143 | |
| NOx Compliance Demonstration | 2.3.2 e) | |
| Turbine Description | axial flow |