|
Aircraft performance |
|
Maximum takeoff weight, kg |
33,000 |
|
Maximum ordnance, kg |
6,500 |
|
Service ceiling (without external ordnance and stores), km |
17 |
|
Maximum flight speed (without external ordnance and stores), km/h |
2,300 |
|
G-limit (operational) |
8 |
|
Maximum flight range, km |
3,000 |
|
Landing approach speed, km/h |
240 |
|
Crew |
1 |
|
Aeroplane dimensions: |
|
|
- length, m |
21.19 |
|
- wingspan, m |
14.7 (7.4*) |
|
- height, m |
5.9 |
|
In-flight refuelling system |
Maximum flow rate
(at entry pressure 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. Fire control system |
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1.1. Search and track radar |
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1.2. IRST and laser rangefinder |
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1.2.1. Optical search and track station |
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1.2.2. Helmet-mounted target designator |
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1.3. IFF system interrogator |
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1.4. Unbiased monitoring system |
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1.5. Wide-angle HUD |
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2. Flight navigation system |
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|
2.1. Attitude and heading reference system |
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2.2. Radiotechnical system for short-range navigation, landing approach and landing of ship-based aircraft |
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2.3. Doppler navigator |
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2.4. GPS system |
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2.5. International navigation system |
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3. Marker radio receiver |
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4. Remote control system |
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5. IFF transponder |
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6.Electronic countermeasure equipment |
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6.1. Radar warning receiver |
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6.2. Chaff and heat flare dispenser |
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6.3. Radio jamming transmitter (in pod) |
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7. Communications system |
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8. Onboard monitoring system |
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9. On-board flight data recording device |
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10. Onboard voice information playback equipment. |
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11. Emergency warning system |
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12. Aircraft responder |
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