| EASA ID |
1PW039 |
|
| Aircraft Engine Manufacturer |
Pratt & Whitney |
Rolls-Royce |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
|
3175 |
| Diameter (mm) |
|
1212 |
| Length (mm) |
|
4039 |
| Wikipedia Article (URL) |
|
en.wikipedia.org/wiki/Rolls-Royce/Snecma_Olympus_593 |
| Fuel |
Jet A |
Jet A1 |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
Nickel alloy construction annular chamber, 16 vaporizing burners, each with twin outlets |
| Afterburner |
No |
Yes |
| Streams |
2 |
1 |
| Bypass Ratio |
6.04 |
|
| Overall Pressure Ratio |
26.9 |
|
| Maximum Takeoff Thrust (kN) |
167.25 |
169.2 |
| Thrust To Weight |
|
5.4 |
| Hydrocarbon Take Off (g/kg fuel) |
0.05 |
|
| Hydrocarbon Climb Out (g/kg fuel) |
0.06 |
|
| Hydrocarbon Approach (g/kg fuel) |
0.21 |
|
| Hydrocarbon Idle (g/kg fuel) |
2.26 |
|
| Hydrocarbon Unitary Average (g/kN) |
3.16 |
|
| Hydrocarbon Unitary Characteristic (g/kN) |
4.9 |
|
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
24.8 |
|
| Hydrocarbon LTO (g) |
530 |
|
| Carbon Monoxide Take Off (g/kg fuel) |
0.4 |
|
| Carbon Monoxide Climb Out (g/kg fuel) |
0.41 |
|
| Carbon Monoxide Approach (g/kg fuel) |
2.3 |
|
| Carbon Monoxide Idle (g/kg fuel) |
23.1 |
|
| Carbon Monoxide Unitary Average (g/kN) |
32 |
|
| Carbon Monoxide Unitary Characteristic (g/kN) |
39.3 |
|
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
33.3 |
|
| NOx Take Off (g/kg fuel) |
31.1 |
|
| NOx Climb Out (g/kg fuel) |
24.8 |
|
| NOx Approach (g/kg fuel) |
10.3 |
|
| NOx Idle (g/kg fuel) |
4.4 |
|
| NOx Unitary Average (g/kN) |
48.1 |
|
| NOx Unitary Characteristic (g/kN) |
55.8 |
|
| NOx Unitaryto Standard (% of limit) |
59.4 |
|
| NOx Unitaryto CAEP2 (% of limit) |
74.3 |
|
| NOx Unitaryto CAEP4 (% of limit) |
89.9 |
|
| NOx Unitaryto CAEP6 (% of limit) |
102.1 |
|
| NOx Unitaryto CAEP8 (% of limit) |
122 |
|
| NOx LTO (g) |
8107 |
|
| Smoke Max (SN) |
11.4 |
|
| Smoke Characteristic (SN) |
14.7 |
|
| Smoke Characteristicto Regulatory (% of limit) |
71.4 |
|
| Fuel Flow Take Off (kg/s) |
1.538 |
|
| Fuel Flow Climbout (kg/s) |
1.266 |
|
| Fuel Flow Approach (kg/s) |
0.399 |
|
| Fuel Flow Idle (kg/s) |
0.141 |
|
| Fuel LTO (kg) |
547 |
|
| Fuel Venting Compliant |
No |
|
| Afterburner Thrust (kN) |
|
169.2 |
| Carbon Monoxide LTO (g) |
5396 |
|
| Compressor Description |
|
Axial-flow, 7-stage low-pressure, 7-stage high-pressure |
| Emissions Data Status |
C |
|
| Emissions Data Superseded |
Yes |
|
| Emissions Superseded By |
4PW072 |
|
| Engine Status |
Out of production |
|
| Turbine Description |
|
Two stages: one high-pressure, one low-pressure |