| Aircraft Engine Manufacturer |
Klimov |
Lyulka-Saturn |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
1055 |
|
| Diameter (mm) |
730 |
|
| Length (mm) |
4229 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Klimov_RD-33 |
en.wikipedia.org/wiki/Lyulka_AL-5 |
| Geared Fan |
No |
No |
| Combustion Chamber |
annular combustor |
annular combustion chamber |
| Afterburner |
Yes |
No |
| Streams |
2 |
1 |
| Bypass Ratio |
0.49 |
|
| Maximum Takeoff Thrust (kN) |
50 |
52 |
| Thrust To Weight |
4.82 |
|
| Specific Fuel Consumption (g/(kN·s)) |
2124.375 |
|
| Compressor Description |
2 spool axial, 4 low pressure stages, 9 high pressure stages |
seven-stage axial-flow |
| Turbine Description |
single stage high pressure, single stage low pressure |
single-stage |