| Tumansky R-25 ✕ | CF34-3A/A1/A2/B1/B2 ✕ | |
|---|---|---|
| EASA ID | 07P05GE220 | |
| Aircraft Engine Manufacturer | Tumansky | General Electric Company |
| Aircraft Engine Type | Turbojet | Turbofan |
| Dry Weight (kg) | 1212 | |
| Diameter (mm) | 1191 | |
| Length (mm) | 4615 | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Tumansky_R-25 | |
| Fuel | Jet A | |
| Geared Fan | No | No |
| Combustion Chamber | Cannular 10 burners | SAC |
| Afterburner | Yes | No |
| Streams | 1 | 2 |
| Bypass Ratio | 6.25 | |
| Overall Pressure Ratio | 19.3 | |
| Maximum Takeoff Thrust (kN) | 40.3 | 41.01 |
| Thrust To Weight | 5.6 | |
| Hydrocarbon Take Off (g/kg fuel) | 0.06 | |
| Hydrocarbon Climb Out (g/kg fuel) | 0.05 | |
| Hydrocarbon Approach (g/kg fuel) | 0.13 | |
| Hydrocarbon Idle (g/kg fuel) | 4.69 | |
| Hydrocarbon Unitary Average (g/kN) | 8.9 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 13.7 | |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 69.9 | |
| Hydrocarbon LTO (g) | 366 | |
| Carbon Monoxide Take Off (g/kg fuel) | 0 | |
| Carbon Monoxide Climb Out (g/kg fuel) | 0 | |
| Carbon Monoxide Approach (g/kg fuel) | 1.88 | |
| Carbon Monoxide Idle (g/kg fuel) | 47.59 | |
| Carbon Monoxide Unitary Average (g/kN) | 89.7 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 110.1 | |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 93.3 | |
| NOx Take Off (g/kg fuel) | 11.28 | |
| NOx Climb Out (g/kg fuel) | 9.68 | |
| NOx Approach (g/kg fuel) | 6.63 | |
| NOx Idle (g/kg fuel) | 3.72 | |
| NOx Unitary Average (g/kN) | 26.3 | |
| NOx Unitary Characteristic (g/kN) | 30.5 | |
| NOx Unitaryto Standard (% of limit) | 38.8 | |
| NOx Unitaryto CAEP2 (% of limit) | 48.5 | |
| NOx Unitaryto CAEP4 (% of limit) | 50.9 | |
| NOx Unitaryto CAEP6 (% of limit) | 52.1 | |
| NOx Unitaryto CAEP8 (% of limit) | 56.4 | |
| NOx LTO (g) | 1078 | |
| Smoke Take Off (SN) | 18.3 | |
| Smoke Climb Out (SN) | 9.2 | |
| Smoke Approach (SN) | 3.1 | |
| Smoke Idle (SN) | 3.1 | |
| Smoke Max (SN) | 18.3 | |
| Smoke Characteristic (SN) | 23.6 | |
| Smoke Characteristicto Regulatory (% of limit) | 78.1 | |
| Fuel Flow Take Off (kg/s) | 0.3991 | |
| Fuel Flow Climbout (kg/s) | 0.3288 | |
| Fuel Flow Approach (kg/s) | 0.116 | |
| Fuel Flow Idle (kg/s) | 0.0489 | |
| Fuel LTO (kg) | 164 | |
| Afterburner Thrust (kN) | 69.6 | |
| Carbon Monoxide LTO (g) | 3683 | |
| Compressor Description | Two-spool axial compressor 3 LP stages, 5 HP stages | |
| Emissions Data Status | C | |
| NOx Compliance Demonstration | 2.3.2 e) | |
| nvPME Imass Approach (mg/kg) | 0.8088 | |
| nvPME Imass Climb Out (mg/kg) | 114.0471 | |
| nvPME Imass Idle (mg/kg) | 1.4487 | |
| nvPME Imass Max (mg/kg) | 287.0006 | |
| nvPME Imass Take Off (mg/kg) | 287.0006 | |
| nvPME Inum Approach (#/kg) | 80427050000000 | |
| nvPME Inum Climb Out (#/kg) | 1333178000000000 | |
| nvPME Inum Idle (#/kg) | 167524400000000 | |
| nvPME Inum Max (#/kg) | 2006645000000000 | |
| nvPME Inum Take Off (#/kg) | 2006645000000000 | |
| nvPMLTO Mass (mg) | 10006.38 | |
| nvPMLTO Mass Per Thrust (mg/kN) | 339.1479 | |
| nvPMLTO Mass To CAEP11 (% of limit) | 35.0526 | |
| nvPMLTO Number (#) | 107382800000000000 | |
| nvPMLTO Number Per Thrust (#/kN) | 3639545000000000 | |
| nvPMLTO Number To CAEP11 (% of limit) | 31.4128 | |
| nvPM Mass Concentration Characteristic (mg/m³) | 10129.73 | |
| nvPM Mass Concentration Max (mg/m³) | 7869.784 | |
| nvPM Mass Concentration To CAEP10 (% of limit) | 90.6489 | |
| Turbine Description | 1 HP stage, 1 LP stage |