|
Aircraft performance |
|
Takeoff weight: |
|
|
- normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg |
24,900* |
|
- maximum, kg |
34,500 |
|
- max, kg |
38,800 |
|
Maximum landing weight, kg |
23,600 |
|
Max landing weight, kg |
30,000 |
|
Maximum internal fuel, kg |
9,640 |
|
Normal internal fuel, kg |
5,270 |
|
Maximum ordnance, kg |
8,000 |
|
Service ceiling (without external ordnance and stores), km |
17.3 |
|
Maximum flight speed at sea level (without external ordnance and stores), km/h |
1,350 |
|
Max Mach (without external ordnance and stores) |
2.00 (1.9**) |
|
G-limit (operational) |
9 |
|
Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance): |
|
|
- at sea level, km |
1,270 |
|
- at height, km |
3,000 |
|
- with one refuelling (at 1.500 kg fuel remaining), km |
5,200 |
|
- with two refuellings in flight, km |
8,000 |
|
Maximum airborne time (pilot-dependent), hours |
10 |
|
Takeoff run at normal takeoff weight, m |
550 |
|
Landing run at normal landing weight (with braking parachute), m |
750 |
|
Aeroplane dimensions: |
|
|
- length, m |
21.9 |
|
- wingspan, m |
14.7 |
|
- height, m |
6.4 |
|
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
(2 x AL-31FP***) |
|
Thrust in afterburner, kgf |
12,500 -2 % |
|
Avionics |
|
1. Fire control system |
|
|
1.1. Air-to-air fire control system |
|
|
1.1.1. Search and track radar |
|
|
1.1.2. IRST and laser rangefinder |
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|
1.1.2.1. Optical search and track station |
|
|
1.1.2.2. Helmet-mounted target designator |
|
|
1.1.3. Wide-angle HUD |
|
|
1.1.4. IFF system interrogator |
|
|
1.2. Air-to-surface fire control system |
|
|
1.2.1. Coloured multi-purpose LCD indicators |
|
|
1.2.2. Onboard digital computer |
|
|
1.2.3. GPS satellite-based navigation system |
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|
1.2.4. Weapons control system |
|
|
2. Aeroplane remote control system |
|
|
3. IFF system transponder |
|
|
4. Antenna feed system |
|
|
5. Flight navigation system |
|
|
5.1. Digital computer |
|
|
5.2. Attitude and heading reference system |
|
|
5.3. Short-range radiotechnical navigation system |
|
|
5.4. GPS system |
|
|
5.5. Autopilot system |
|
|
5.6. Altitude and speed data processing and display system |
|
|
5.7. Air data system |
|
|
6. Electronic countermeasure equipment |
|
|
6.1. Radar warning receiver with an expansion block |
|
|
6.2. Chaff and heat flare dispenser |
|
|
6.3. Radio jamming transmitter (in pod) |
|
|
7. Communications system |
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|
7.1. VHF and UHF band communications transceiver |
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7.2. VHF and UHF band communications transceiver |
|
|
7.3. SW band radio communications transceiver |
|
|
8. Onboard automatic control system |
|
|
8.1. Integrated onboard control and crew warning system |
|
|
8.2. Flight information recording equipment |
|
|
8.3. Onboard emergency situation warning equipment |
|
|
9. Video recording system |
|
|
9.1. Onboard video recorder |
|
|
9.2. Forward vision video camera |
|
|
9.3. Video controller |
|
|
10. Aircraft responder |
|
|
11. Telecommand homing system |
|
|
12. Pod-type IRST and laser rangefinder |
|
|
Limits |
|
Aircraft limit: |
|
|
- SLL, hours |
3,000 |
|
- to first overhaul, hours |
1,500 |
|
- service life, years |
25 |
|
Engine and outboard accessory-gearbox life: |
|
|
- to first overhaul, hours |
500 |
|
- service life limit, hours |
1,500 |
