| EASA ID |
|
1PW038 |
| Aircraft Engine Manufacturer |
Lyulka-Saturn |
Pratt & Whitney Canada |
| Aircraft Engine Type |
Turbojet |
Turbofan |
| Dry Weight (kg) |
885 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Lyulka_TR-1 |
|
| Fuel |
|
Jet A-1 |
| Geared Fan |
No |
No |
| Afterburner |
No |
No |
| Streams |
1 |
2 |
| Bypass Ratio |
|
2.1 |
| Overall Pressure Ratio |
|
13.3 |
| Maximum Takeoff Thrust (kN) |
12.8 |
14.19 |
| Thrust To Weight |
1.47 |
|
| Specific Fuel Consumption (g/(kN·s)) |
3653.925 |
|
| 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 |
eight-stage axial-flow |
|
| Emissions Data Status |
|
C |
| Engine Status |
|
Out of production |
| Turbine Description |
single stage |
|