PW1130G-JM

Maximum Takeoff Thrust
134 kN
Bypass Ratio
11.7
Overall Pressure Ratio
35.52
Fuel Flow Take Off
0.910084 kg/s
NOx Unitaryto CAEP8
56.09 % of limit

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan Yes 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 TALON X
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 11.7 Overall Pressure Ratio 35.52 Afterburner No

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Airplanes

Name Model Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Two Class Typical Seating Max Seating
A321-272N A321neo PW1130G-JM 2 44.51 35.8 206 244
A321-272NX A321neo PW1130G-JM 2 44.51 35.8 206 244

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
PW1428GH-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
PW1428GA-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
PW1428G-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
PW1129G-JM Pratt & Whitney 130.08 12 34.02 Compare
PW1431GH-JM Pratt & Whitney 140.4386 11.8646 35.59 Compare
PW1431GA-JM Pratt & Whitney 140.4386 11.8646 35.59 Compare
All data (56 fields)
Name
PW1130G-JM
EASA ID
15PW106
Aircraft Engine Manufacturer
Pratt & Whitney
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
Yes
Combustion Chamber
TALON X
Afterburner
No
Streams
2
Bypass Ratio
11.7
Overall Pressure Ratio
35.52
Maximum Takeoff Thrust (kN)
134
Hydrocarbon Take Off (g/kg fuel)
0.03
Hydrocarbon Climb Out (g/kg fuel)
0.03
Hydrocarbon Approach (g/kg fuel)
0.04
Hydrocarbon Idle (g/kg fuel)
0.07
Hydrocarbon Unitary Average (g/kN)
0.1
Hydrocarbon Unitary Characteristic (g/kN)
0.2
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
1.02
Hydrocarbon LTO (g)
18
Carbon Monoxide Take Off (g/kg fuel)
0.17
Carbon Monoxide Climb Out (g/kg fuel)
0.25
Carbon Monoxide Approach (g/kg fuel)
4.55
Carbon Monoxide Idle (g/kg fuel)
19.48
Carbon Monoxide Unitary Average (g/kN)
23.7
Carbon Monoxide Unitary Characteristic (g/kN)
29.1
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
24.66
NOx Take Off (g/kg fuel)
21.16
NOx Climb Out (g/kg fuel)
16.33
NOx Approach (g/kg fuel)
8.99
NOx Idle (g/kg fuel)
6.78
NOx Unitary Average (g/kN)
29.6
NOx Unitary Characteristic (g/kN)
34.3
NOx Unitaryto Standard (% of limit)
30.89
NOx Unitaryto CAEP2 (% of limit)
38.61
NOx Unitaryto CAEP4 (% of limit)
43.95
NOx Unitaryto CAEP6 (% of limit)
49
NOx Unitaryto CAEP8 (% of limit)
56.09
NOx LTO (g)
3969
Smoke Take Off (SN)
2.8
Smoke Climb Out (SN)
0.79
Smoke Approach (SN)
0.35
Smoke Idle (SN)
0.55
Smoke Max (SN)
2.8
Smoke Characteristic (SN)
3.6
Smoke Characteristicto Regulatory (% of limit)
16.48
Fuel Flow Take Off (kg/s)
0.910084
Fuel Flow Climbout (kg/s)
0.748352
Fuel Flow Approach (kg/s)
0.254698
Fuel Flow Idle (kg/s)
0.094272
Fuel LTO (kg)
345.2
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
3174
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)