|
Aircraft performance |
Takeoff weight:
- normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg
- maximum, kg |
23,430*
30,450 |
|
Maximum landing weight, kg |
21,000 |
|
Max landing weight, kg |
23,000 |
|
Maximum internal fuel, kg |
9,400 |
|
Maximum ordnance, kg |
4,430 |
|
Service ceiling (without external ordnance and stores), km |
18.5 |
|
Maximum flight speed at sea level (without external ordnance and stores), km/h |
1,400 |
|
Max Mach (without external ordnance and stores) |
2.35 |
|
G-limit (operational) |
9 |
Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance):
- at sea level, km
- at height, km |
1,340
3,530 |
|
Maximum airborne time, hours |
4.5 |
|
Take-off run at normal takeoff weight, m |
450 |
|
Landing run at normal landing weight (with braking parachute), m |
620 |
Aircraft dimensions:
- length, m
- wingspan, m
- height, m |
21.9
14.7
5.9 |
|
Crew |
1 |
|
Powerplant |
|
Number and type of engines |
2 x AL-31F |
Thrust:
- in afterburner, kgf
- at full power, kgf |
12,500 -2 %
7,670 ± 2 % |
|
Avionics |
|
1. Fire control system: |
|
|
1.1. Search and track radar |
|
|
1.2. IRST and laser rangefinder linked to pilot's helmet-mounted target designator |
|
|
1.3. Wide-angle HUD |
|
|
1.4. IFF system interrogator |
|
|
1.5. Weapons control system |
|
|
2. Remote control system |
|
|
3. IFF system transponder |
|
|
4. Antenna feed system |
|
|
5. Flight navigation system composed of: |
|
|
5.1. Navigation system composed of: |
|
|
5.1.1. Digital computer |
|
|
5.1.2. Attitude and heading reference system |
|
|
5.1.3. Short-range radiotechnical navigation system (SRRNS) |
|
|
5.1.4. Automatic direction finder |
|
|
5.2. Autopilot system |
|
|
5.3. Altitude and speed data processing and display system |
|
|
6. GPS satellite-based navigation system |
|
|
7. Marker radio receiver |
|
|
8. Electronic countermeasure equipment |
|
|
8.1. Radar warning receiver |
|
|
8.2. Chaff and heat flare dispenser |
|
|
8.3. Radio jamming transmitter (in pod) |
|
|
9. Communications system, including |
|
|
9.1. VHF and UHF band communications transceiver |
|
|
9.2. VHF and UHF band communications transceiver |
|
|
9.3. SW band radio communications transceiver |
|
|
9.4. Data communication terminal equipment |
|
|
10. Onboard automatic monitoring system |
|
|
10.1. Integrated onboard early warning system |
|
|
10.2. Flight information recording equipment with operational storage unit |
|
|
10.3. Onboard emergency situation warning equipment |
|
|
10.4. Emergency warning system |
|
|
10.5. Onboard recording device |
|
|
11. Aircraft responder |
|
|
Limits |
|
A limit: |
|
|
- SLL, hours |
2,000 |
|
- to first overhaul, hours |
1,000 |
|
- service life, years |
20 |
|
Engine and outboard accessory-gearbox life: |
|
|
- to first overhaul, hours |
300 |
|
- service life limit, hours |
900 |
