Trent 1000-G

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

323.7 kN

Bypass Ratio

9.39

Overall Pressure Ratio

42.53

Fuel Flow Take Off

2.403 kg/s

NOx Unitaryto CAEP8

83.6 % 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 9.39	Overall Pressure Ratio 42.53	Afterburner No

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Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
Trent 1000-G	Rolls-Royce	323.7	9.39	42.53	Compare
Trent 1000-G2	Rolls-Royce	323.7	9.23	42.81	Compare
Trent 1000-G3	Rolls-Royce	323.7283	9.1084	43.893	Compare
Trent7000-72	Rolls-Royce	327.914	9.0559	44.62	Compare
Trent7000-72C	Rolls-Royce	327.914	9.0559	44.62	Compare
Trent7000-72D	Rolls-Royce	327.914	9.0559	44.62	Compare

All data (65 fields)

Name: Trent 1000-G
EASA ID: 11RR053
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Geared Fan: No
Combustion Chamber: Phase5 Tiled
Afterburner: No
Streams: 2
Bypass Ratio: 9.39
Overall Pressure Ratio: 42.53
Maximum Takeoff Thrust (kN): 323.7
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): 0.05
Hydrocarbon Unitary Average (g/kN): 0.05
Hydrocarbon Unitary Sigma (g/kN): 0.045
Hydrocarbon Unitary Range (g/kN): 0-0.1
Hydrocarbon Unitary Characteristic (g/kN): 0.06
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 0.3
Hydrocarbon LTO (g): 17
Carbon Monoxide Take Off (g/kg fuel): 0.53
Carbon Monoxide Climb Out (g/kg fuel): 0.47
Carbon Monoxide Approach (g/kg fuel): 0.72
Carbon Monoxide Idle (g/kg fuel): 8.14
Carbon Monoxide Unitary Average (g/kN): 10.37
Carbon Monoxide Unitary SD (g/kN): 3
Carbon Monoxide Unitary Range (g/kN): 6.3-13
Carbon Monoxide Unitary Characteristic (g/kN): 11.22
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 9.5
NOx Take Off (g/kg fuel): 50.27
NOx Climb Out (g/kg fuel): 38.18
NOx Approach (g/kg fuel): 13.6
NOx Idle (g/kg fuel): 5.54
NOx Unitary Average (g/kN): 59.31
NOx Unitary SD (g/kN): 0.92
NOx Unitary Range (g/kN): 58.4-60.5
NOx Unitary Characteristic (g/kN): 62.82
NOx Unitaryto Standard (% of limit): 50.2
NOx Unitaryto CAEP2 (% of limit): 62.8
NOx Unitaryto CAEP4 (% of limit): 68.2
NOx Unitaryto CAEP6 (% of limit): 74.8
NOx Unitaryto CAEP8 (% of limit): 83.6
NOx LTO (g): 19198
Smoke Take Off (SN): 3.1
Smoke Climb Out (SN): 3.9
Smoke Approach (SN): 3
Smoke Idle (SN): 0.6
Smoke Max (SN): 5.2
Smoke Sigma (SN): 1.99
Smoke Range (SN): 3-8.2
Smoke Characteristic (SN): 5.75
Smoke Characteristicto Regulatory (% of limit): 33.5
Fuel Flow Take Off (kg/s): 2.403
Fuel Flow Climbout (kg/s): 1.968
Fuel Flow Approach (kg/s): 0.649
Fuel Flow Idle (kg/s): 0.242
Fuel LTO (kg): 75
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 3358
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 12RR059
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 d)