Maximum Takeoff Thrust
350.9024 kN
Overall Pressure Ratio
47.9558
Fuel Flow Take Off
2.7209 kg/s
NOx Unitaryto CAEP8
85.9695 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
Phase5 Tiled |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
8.9342 |
Overall Pressure Ratio
47.9558 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- Trent 1000-J3
- EASA ID
- 02P23RR131
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.9342
- Overall Pressure Ratio
- 47.9558
- Maximum Takeoff Thrust (kN)
- 350.9024
- 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)
- 0
- Hydrocarbon Unitary Average (g/kN)
- 0
- Hydrocarbon Unitary Sigma (g/kN)
- 0
- Hydrocarbon Unitary Range (g/kN)
- 0-0
- Hydrocarbon Unitary Characteristic (g/kN)
- 0
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 0
- Hydrocarbon LTO (g)
- 0
- Carbon Monoxide Take Off (g/kg fuel)
- 0.3729
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.4322
- Carbon Monoxide Approach (g/kg fuel)
- 0.5519
- Carbon Monoxide Idle (g/kg fuel)
- 6.0143
- Carbon Monoxide Unitary Average (g/kN)
- 7.8013
- Carbon Monoxide Unitary SD (g/kN)
- 1.5631
- Carbon Monoxide Unitary Range (g/kN)
- 5.03-9.78
- Carbon Monoxide Unitary Characteristic (g/kN)
- 8.18
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 6.9
- NOx Take Off (g/kg fuel)
- 60.6796
- NOx Climb Out (g/kg fuel)
- 44.9155
- NOx Approach (g/kg fuel)
- 14.6824
- NOx Idle (g/kg fuel)
- 5.9679
- NOx Unitary Average (g/kN)
- 71.4314
- NOx Unitary SD (g/kN)
- 1.1218
- NOx Unitary Range (g/kN)
- 69.37-72.61
- NOx Unitary Characteristic (g/kN)
- 73.9609
- NOx Unitaryto Standard (% of limit)
- 54.4184
- NOx Unitaryto CAEP2 (% of limit)
- 68.023
- NOx Unitaryto CAEP4 (% of limit)
- 71.8684
- NOx Unitaryto CAEP6 (% of limit)
- 77.959
- NOx Unitaryto CAEP8 (% of limit)
- 85.9695
- NOx LTO (g)
- 25064.2
- Smoke Take Off (SN)
- 7.6822
- Smoke Climb Out (SN)
- 10.4388
- Smoke Approach (SN)
- 9.77
- Smoke Idle (SN)
- 1.8312
- Smoke Max (SN)
- 14.7
- Smoke Sigma (SN)
- 2
- Smoke Range (SN)
- 11.4-16.7
- Smoke Characteristic (SN)
- 16.4
- Smoke Characteristicto Regulatory (% of limit)
- 97.7
- Fuel Flow Take Off (kg/s)
- 2.7209
- Fuel Flow Climbout (kg/s)
- 2.2169
- Fuel Flow Approach (kg/s)
- 0.7186
- Fuel Flow Idle (kg/s)
- 0.2636
- Fuel LTO (kg)
- 990.5745
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2737.355
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 80.9354
- nvPME Imass Climb Out (mg/kg)
- 65.3419
- nvPME Imass Idle (mg/kg)
- 19.3164
- nvPME Imass Max (mg/kg)
- 153.6664
- nvPME Imass Take Off (mg/kg)
- 41.5701
- nvPME Inum Approach (#/kg)
- 884413000000000
- nvPME Inum Climb Out (#/kg)
- 210951100000000
- nvPME Inum Idle (#/kg)
- 467588700000000
- nvPME Inum Max (#/kg)
- 930730000000000
- nvPME Inum Take Off (#/kg)
- 110833800000000
- nvPMLTO Mass (mg)
- 45772.86
- nvPMLTO Mass Per Thrust (mg/kN)
- 181.3223
- nvPMLTO Mass To CAEP11 (% of limit)
- 84.73
- nvPMLTO Number (#)
- 419198800000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1660593000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 59.7336
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 89.2488