Compare reaction turbines
All reaction turbines
|
Trent 1000-H3
✕
|
Trent 1000-H2
✕
|
| EASA ID |
02P23RR130 |
12RR066 |
| Aircraft Engine Manufacturer |
Rolls-Royce |
Rolls-Royce |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Geared Fan |
No |
No |
| Combustion Chamber |
Phase5 Tiled |
Phase5 Tiled |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
9.282 |
9.49 |
| Overall Pressure Ratio |
40.3476 |
38.52 |
| Maximum Takeoff Thrust (kN) |
287.1372 |
287.1 |
| Hydrocarbon Take Off (g/kg fuel) |
0 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0 |
0 |
| Hydrocarbon Approach (g/kg fuel) |
0 |
0 |
| Hydrocarbon Idle (g/kg fuel) |
0 |
0.07 |
| Hydrocarbon Unitary Average (g/kN) |
0 |
0.09 |
| Hydrocarbon Unitary Sigma (g/kN) |
0 |
0.08 |
| Hydrocarbon Unitary Range (g/kN) |
0-0 |
0-0.17 |
| Hydrocarbon Unitary Characteristic (g/kN) |
0 |
0.1 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
0 |
0.5 |
| Hydrocarbon LTO (g) |
0 |
24.81 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.427 |
0.48 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.385 |
0.43 |
| Carbon Monoxide Approach (g/kg fuel) |
0.8262 |
0.89 |
| Carbon Monoxide Idle (g/kg fuel) |
8.3928 |
9.82 |
| Carbon Monoxide Unitary Average (g/kN) |
11.4447 |
13.35 |
| Carbon Monoxide Unitary SD (g/kN) |
2.0505 |
3.36 |
| Carbon Monoxide Unitary Range (g/kN) |
7.4-14.1 |
9.37-17.18 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
12 |
14.28 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
10.2 |
12.1 |
| NOx Take Off (g/kg fuel) |
42.1376 |
40.46 |
| NOx Climb Out (g/kg fuel) |
32.826 |
31.49 |
| NOx Approach (g/kg fuel) |
13.0422 |
12.56 |
| NOx Idle (g/kg fuel) |
5.2915 |
5.21 |
| NOx Unitary Average (g/kN) |
52.3346 |
49.8 |
| NOx Unitary SD (g/kN) |
0.892 |
0.77 |
| NOx Unitary Range (g/kN) |
50.9-53.47 |
49.13-50.61 |
| NOx Unitary Characteristic (g/kN) |
54.1879 |
52.34 |
| NOx Unitaryto Standard (% of limit) |
44.8965 |
44.72 |
| NOx Unitaryto CAEP2 (% of limit) |
56.1206 |
55.9 |
| NOx Unitaryto CAEP4 (% of limit) |
61.7912 |
62.28 |
| NOx Unitaryto CAEP6 (% of limit) |
68.0281 |
68.86 |
| NOx Unitaryto CAEP8 (% of limit) |
76.5202 |
77.93 |
| NOx LTO (g) |
15026.47 |
14299 |
| Smoke Take Off (SN) |
11.1422 |
3.8 |
| Smoke Climb Out (SN) |
13.7777 |
4.8 |
| Smoke Approach (SN) |
7.6908 |
3.3 |
| Smoke Idle (SN) |
2.1653 |
0.5 |
| Smoke Max (SN) |
14.7 |
5.98 |
| Smoke Sigma (SN) |
2 |
2.26 |
| Smoke Range (SN) |
11.4-16.7 |
3-8.3 |
| Smoke Characteristic (SN) |
16.4 |
6.5 |
| Smoke Characteristicto Regulatory (% of limit) |
92.4 |
36.64 |
| Fuel Flow Take Off (kg/s) |
2.1075 |
2.075 |
| Fuel Flow Climbout (kg/s) |
1.7323 |
1.715 |
| Fuel Flow Approach (kg/s) |
0.5983 |
0.582 |
| Fuel Flow Idle (kg/s) |
0.2323 |
0.233 |
| Fuel LTO (kg) |
823.1809 |
817 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
3286.042 |
3832 |
| Emissions Data Status |
C |
C |
| Engine Status |
Out of production |
Out of production |
| NOx Compliance Demonstration |
2.3.2 e) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
64.1533 |
|
| nvPME Imass Climb Out (mg/kg) |
114.0449 |
|
| nvPME Imass Idle (mg/kg) |
18.3136 |
|
| nvPME Imass Max (mg/kg) |
150.392 |
|
| nvPME Imass Take Off (mg/kg) |
71.5551 |
|
| nvPME Inum Approach (#/kg) |
811570200000000 |
|
| nvPME Inum Climb Out (#/kg) |
417370300000000 |
|
| nvPME Inum Idle (#/kg) |
434505600000000 |
|
| nvPME Inum Max (#/kg) |
918210000000000 |
|
| nvPME Inum Take Off (#/kg) |
236022300000000 |
|
| nvPMLTO Mass (mg) |
48260.9 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
233.6337 |
|
| nvPMLTO Mass To CAEP11 (% of limit) |
109.1746 |
|
| nvPMLTO Number (#) |
390335500000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
1889636000000000 |
|
| nvPMLTO Number To CAEP11 (% of limit) |
67.9725 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
3409.81 |
|
| nvPM Mass Concentration Max (mg/m³) |
2649.081 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
82.7371 |
|