| Tumansky RD-9 ✕ | HTF7500E (AS907-3-1E-A1) ✕ | |
|---|---|---|
| EASA ID | 14HN006 | |
| Aircraft Engine Manufacturer | Shenyang | Honeywell |
| 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 | |
| Geared Fan | No | No |
| Combustion Chamber | SABER-1 | |
| Afterburner | Yes | No |
| Streams | 1 | 2 |
| Bypass Ratio | 4.2 | |
| Overall Pressure Ratio | 21.05 | |
| Maximum Takeoff Thrust (kN) | 29 | 29.4 |
| Thrust To Weight | 5.2 | |
| Hydrocarbon Take Off (g/kg fuel) | 0.06 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0.07 | |
| Hydrocarbon Approach (g/kg fuel) | 0.12 | |
| Hydrocarbon Idle (g/kg fuel) | 1.31 | |
| Hydrocarbon Unitary Average (g/kN) | 3.52 | |
| Hydrocarbon Unitary Sigma (g/kN) | 0.68 | |
| Hydrocarbon Unitary Range (g/kN) | 2.55-4.63 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 4.11 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 21 | |
| Hydrocarbon LTO (g) | 104 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0.56 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.73 | |
| Carbon Monoxide Approach (g/kg fuel) | 6.83 | |
| Carbon Monoxide Idle (g/kg fuel) | 34.64 | |
| Carbon Monoxide Unitary Average (g/kN) | 94.11 | |
| Carbon Monoxide Unitary SD (g/kN) | 3.95 | |
| Carbon Monoxide Unitary Range (g/kN) | 88-99.4 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 101.79 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 86.3 | |
| NOx Take Off (g/kg fuel) | 17.11 | |
| NOx Climb Out (g/kg fuel) | 15.59 | |
| NOx Approach (g/kg fuel) | 8.45 | |
| NOx Idle (g/kg fuel) | 3.83 | |
| NOx Unitary Average (g/kN) | 42.89 | |
| NOx Unitary SD (g/kN) | 2.1 | |
| NOx Unitary Range (g/kN) | 37.49-44.6 | |
| NOx Unitary Characteristic (g/kN) | 45.43 | |
| NOx Unitaryto Standard (% of limit) | 55.3 | |
| NOx Unitaryto CAEP2 (% of limit) | 69.2 | |
| NOx Unitaryto CAEP4 (% of limit) | 69.8 | |
| NOx Unitaryto CAEP6 (% of limit) | 70.1 | |
| NOx Unitaryto CAEP8 (% of limit) | 74.1 | |
| NOx LTO (g) | 1263 | |
| Smoke Take Off (SN) | 13.6 | |
| Smoke Climb Out (SN) | 8.8 | |
| Smoke Approach (SN) | 0.7 | |
| Smoke Idle (SN) | 1.74 | |
| Smoke Max (SN) | 13.6 | |
| Smoke Sigma (SN) | 1.59 | |
| Smoke Range (SN) | 9-13.6 | |
| Smoke Characteristic (SN) | 15 | |
| Smoke Characteristicto Regulatory (% of limit) | 45.2 | |
| Fuel Flow Take Off (kg/s) | 0.32 | |
| Fuel Flow Climbout (kg/s) | 0.267 | |
| Fuel Flow Approach (kg/s) | 0.097 | |
| Fuel Flow Idle (kg/s) | 0.048 | |
| Fuel LTO (kg) | 147 | |
| Fuel Venting Compliant | Yes | |
| Afterburner Thrust (kN) | 37 | |
| Carbon Monoxide LTO (g) | 2786 | |
| Compressor Description | Single-spool 9-stage Axial compressor | |
| Emissions Data Status | C | |
| Emissions Data Superseded | Yes | |
| Emissions Superseded By | 01P14HN014 | |
| NOx Compliance Demonstration | 2.3.2 e) | |
| Turbine Description | axial flow |