| EASA ID |
1PW038 |
|
| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
Heinkel-Hirth |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
|
950 |
| Diameter (mm) |
|
875 |
| Length (mm) |
|
3405 |
| Wikipedia Article (URL) |
|
en.wikipedia.org/wiki/Heinkel_HeS_011 |
| Fuel |
Jet A-1 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
|
16 chamber annular |
| Afterburner |
No |
No |
| Streams |
2 |
1 |
| Bypass Ratio |
2.1 |
|
| Overall Pressure Ratio |
13.3 |
|
| Maximum Takeoff Thrust (kN) |
14.19 |
12.7 |
| Thrust To Weight |
|
1.38 |
| Hydrocarbon Take Off (g/kg fuel) |
0 |
|
| Hydrocarbon Climb Out (g/kg fuel) |
0.67 |
|
| Hydrocarbon Approach (g/kg fuel) |
16 |
|
| Hydrocarbon Idle (g/kg fuel) |
96.67 |
|
| Hydrocarbon Unitary Average (g/kN) |
312.8 |
|
| Hydrocarbon Unitary Characteristic (g/kN) |
481.7 |
|
| Hydrocarbon LTO (g) |
4439 |
|
| Carbon Monoxide Take Off (g/kg fuel) |
2.52 |
|
| Carbon Monoxide Climb Out (g/kg fuel) |
4.18 |
|
| Carbon Monoxide Approach (g/kg fuel) |
49.24 |
|
| Carbon Monoxide Idle (g/kg fuel) |
124.6 |
|
| Carbon Monoxide Unitary Average (g/kN) |
443.1 |
|
| Carbon Monoxide Unitary Characteristic (g/kN) |
543.9 |
|
| NOx Take Off (g/kg fuel) |
9.93 |
|
| NOx Climb Out (g/kg fuel) |
9.79 |
|
| NOx Approach (g/kg fuel) |
5.23 |
|
| NOx Idle (g/kg fuel) |
1.08 |
|
| NOx Unitary Average (g/kN) |
32 |
|
| NOx Unitary Characteristic (g/kN) |
37.1 |
|
| NOx LTO (g) |
454 |
|
| Smoke Take Off (SN) |
17.1 |
|
| Smoke Climb Out (SN) |
15.1 |
|
| Smoke Max (SN) |
17.1 |
|
| Smoke Sigma (SN) |
2.23 |
|
| Smoke Range (SN) |
15.5-17.1 |
|
| Smoke Characteristic (SN) |
20.1 |
|
| Fuel Flow Take Off (kg/s) |
0.2151 |
|
| Fuel Flow Climbout (kg/s) |
0.1802 |
|
| Fuel Flow Approach (kg/s) |
0.0678 |
|
| Fuel Flow Idle (kg/s) |
0.0276 |
|
| Fuel LTO (kg) |
92 |
|
| Fuel Venting Compliant |
No |
|
| Carbon Monoxide LTO (g) |
6288 |
|
| Compressor Description |
|
Diagonal + 3-stage axial |
| Emissions Data Status |
C |
|
| Engine Status |
Out of production |
|
| Turbine Description |
|
2-stage axial |