Trent 1000-G2

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

323.7 kN

Bypass Ratio

9.23

Overall Pressure Ratio

42.81

Fuel Flow Take Off

2.402 kg/s

NOx Unitaryto CAEP8

81.67 % 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 9.23	Overall Pressure Ratio 42.81	Afterburner No

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Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
Trent 1000-G3	Rolls-Royce	323.7283	9.1084	43.893	Compare
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All data (63 fields)

Name: Trent 1000-G2
EASA ID: 12RR065
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Geared Fan: No
Combustion Chamber: Phase5 Tiled
Afterburner: No
Streams: 2
Bypass Ratio: 9.23
Overall Pressure Ratio: 42.81
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): 0.04
Hydrocarbon Unitary Average (g/kN): 0.04
Hydrocarbon Unitary Sigma (g/kN): 0.04
Hydrocarbon Unitary Range (g/kN): 0-0.09
Hydrocarbon Unitary Characteristic (g/kN): 0.05
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 0.24
Hydrocarbon LTO (g): 13.56
Carbon Monoxide Take Off (g/kg fuel): 0.51
Carbon Monoxide Climb Out (g/kg fuel): 0.46
Carbon Monoxide Approach (g/kg fuel): 0.72
Carbon Monoxide Idle (g/kg fuel): 7.81
Carbon Monoxide Unitary Average (g/kN): 10.02
Carbon Monoxide Unitary SD (g/kN): 2.66
Carbon Monoxide Unitary Range (g/kN): 6.81-12.98
Carbon Monoxide Unitary Characteristic (g/kN): 10.72
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 9.08
NOx Take Off (g/kg fuel): 49.57
NOx Climb Out (g/kg fuel): 37.8
NOx Approach (g/kg fuel): 13.41
NOx Idle (g/kg fuel): 5.62
NOx Unitary Average (g/kN): 58.87
NOx Unitary SD (g/kN): 0.85
NOx Unitary Range (g/kN): 58.03-59.78
NOx Unitary Characteristic (g/kN): 61.87
NOx Unitaryto Standard (% of limit): 49.25
NOx Unitaryto CAEP2 (% of limit): 61.56
NOx Unitaryto CAEP4 (% of limit): 66.79
NOx Unitaryto CAEP6 (% of limit): 73.14
NOx Unitaryto CAEP8 (% of limit): 81.67
NOx LTO (g): 19058
Smoke Take Off (SN): 3.3
Smoke Climb Out (SN): 4
Smoke Approach (SN): 3.8
Smoke Idle (SN): 0.5
Smoke Max (SN): 5.98
Smoke Sigma (SN): 2.26
Smoke Range (SN): 3-8.3
Smoke Characteristic (SN): 6.5
Smoke Characteristicto Regulatory (% of limit): 37.86
Fuel Flow Take Off (kg/s): 2.402
Fuel Flow Climbout (kg/s): 1.973
Fuel Flow Approach (kg/s): 0.647
Fuel Flow Idle (kg/s): 0.243
Fuel LTO (kg): 895
Fuel Venting Compliant: Yes
Carbon Monoxide LTO (g): 3242
Emissions Data Status: C
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)