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Aircraft performance |
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Takeoff weight: |
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|
- normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg |
23,900* |
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- maximum, kg |
33,000 |
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Maximum landing weight, kg |
21,000 |
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Max landing weight, kg |
23,000 |
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Maximum internal fuel, kg |
9,400 |
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Maximum ordnance, kg |
4,430 |
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Service ceiling (without appendages), km |
17.5 |
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Maximum flight speed at sea level (without external ordnance and stores, km/h |
1,400 |
|
Max Mach (without external ordnance and stores) |
2.0 |
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G-limit (operational) |
9 |
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Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance): |
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- at sea level, km |
1,270 |
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- at height, km |
3,000 |
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Maximum airborne time, hours |
4.5 |
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Takeoff run at normal takeoff weight, m |
550 |
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Landing run at normal landing weight (with braking parachute), m |
670 |
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Aircraft dimensions: |
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- length, m |
21.9 |
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- wingspan, m |
14.7 |
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- height, m |
6.4 |
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Crew |
2 |
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Powerplant |
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Number and type of engines |
2 x AL-31F |
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Thrust: |
|
|
- in afterburner, kgf |
12,500 -2 % |
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- at full power, kgf |
7,670 ± 2 % |
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Avionics |
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1. Fire control system (to be upgraded for use of RVV-AYe rocket) |
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1.1 Search and track radar (to be upgraded for use of new ADO types) |
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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. Wide-angle HUD |
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2. Fire control system (to be upgraded for use of new ADO types) |
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3. GPS satellite-based navigation system |
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4. Flight navigation system |
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4.1. Attitude and heading reference system |
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4.2. Short-range radio navigation system |
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4.3. Autopilot system |
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4.4. Radio altimeter |
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4.5. Air data system |
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4.6. Limiting signal system |
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5. IFF system transponder |
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6. Communications system |
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6.1. VHF/UHF-band communications transceiver |
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6.2. SW band radio communications transceiver |
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6.3. Data communication terminal equipment |
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7. Electronic countermeasure equipment |
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7.1. Radar warning receiver |
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7.2. Radio jamming transmitter (in pod) |
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7.3. Chaff and heat flare dispenser |
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8. Monitoring and recording system |
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8.1. Integrated onboard control and crew warning system |
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8.2. Flight information recording equipment |
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8.3. Onboard emergency situation warning equipment |
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8.4. Emergency warning system |
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9. Aircraft responder |
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10. Command guidance equipment |
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Limits |
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Aircraft limit: |
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- SLL, hours |
2,000 |
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- to first overhaul, hours |
1,000 |
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- service life, years |
20 |
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Engine and outboard accessory-gearbox life: |
|
|
- to first overhaul, hours |
300 |
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- service life limit, hours |
900 |
