.jpg "Saturn AL-31F series 42 (M1) Turbofan engine © Konstantinos Panitsidis")
In numbers Through the lens Video
The Saturn Al-31F Series 42 (M1) military turbofan engines, with afterburner and TVC (Thrust Vector Control).
.jpg "Saturn Al-31F Series 42 (M1), TVC (Thrust Vector Control) © Konstantinos Panitsidis") |
| Technical characteristics of the nozzle | |
| Constructing | Module-construction engine consists of the following main assemblies (modules) |
| Maximum thrust with afterburner, kgf | 13.500 |
| Thrust Vector Control, with its movement, degrees | 16 for all axes |
| Nozzle deflection rate, deg/s | 45 |
| Diameter engine ((inlet), m | 0,92 |
| Length engine, m | 4,99 |
| Maximum diameter engine for hydraulic drives, with Thrust Vector Control, m | 1,33 |
| Engine weight (with Thrust Vector Control and etc.), kg | 2.100+2% |
Technical specifications
| DESIGNER | Lyulka (NPO Saturn) |
| COUNTRY | Russia |
| TYPE |
Turbofan engine
|
| Installed On (aerial means) |
Su-27 and all its versions, OK-GKI BTS-02
|
| Fuel |
-
|
| Oil | - |
| Maximum thrust take-off power rating | 13.500 kgf |
| Specific fuel consumption, take-off power rating | - |
| Maximum thrust, cruise power | - |
| Specific fuel consumption, cruise power | 0,685 kg/kgf*h |
| Pressure ratio, take-off power rating | - |
| Bypass ratio | - |
| Temperature of the gas at the turbine intake, take-off power rating | - |
| Air flow rate, take-off power rating | - |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | - |
| OVERALL DIMENSIONS | |
| Diameter | 924 mm |
| Height | - |
| Width | 1140 mm |
| Length | 4945 mm |
| WEIGHT | |
| Engine weight | 1.520 kg |
| Overhaul operation time | - |
| Specified service life | - |
| Shelf life of preserved engine | - |
Photos AL-31F Series 42 (M1) Turbofan engine
