|
Aircraft performance |
|
Normal takeoff mass, kg |
38,240 |
|
Maximum ordnance, kg |
8,000 |
|
Service ceiling (without external ordnance and stores), km |
15 |
|
Maximum flight speed at sea level (without external ordnance and stores), km/h |
1,400 |
|
Maximum flight speed at altitude (without external ordnance and stores), km/h |
1,900 |
|
G-limit (operational) |
9 |
|
Maximum range, km |
1,100 |
|
Ferry range, km |
4,000 |
|
Maximum airborne time (pilot-dependent), hours |
10 |
|
Aeroplane dimensions: |
|
|
- length, m |
23.34 |
|
- wingspan, m |
14.7 |
|
- height, m |
6.09 |
|
Crew |
2 |
|
In-flight refuelling system |
|
Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min |
1,100 |
|
Powerplant |
|
Number and type of engines |
2 x AL-31F |
|
Thrust in afterburner, kgf |
12,500 -2 % |
|
Avionics |
|
1. Avionics |
|
|
1.1. Electronic countermeasures suite |
|
|
1.2. Multi-purpose forward-looking PAA radar |
|
|
2. Optical-electronic attack and navigation system |
|
|
2.1. Information visualisation system |
|
|
2.2. Onboard graphics station |
|
|
2.3. Laser/TV station |
|
|
3. Aeroplane control system |
|
|
3.1. Autopilot system |
|
|
3.2. Remote control system |
|
|
4. Communications system |
|
|
5. Integrated defensive aids suite |
|
|
6. Kh-59ME missile preparation and telecommand homing equipment pod |
|
|
7. Monitoring and recording system |
|
|
7.1. Onboard automatic monitoring and display system |
|
|
7.2. Unbiased monitoring equipment |
|
|
7.3. Flight information recording equipment |
|
