|
Aircraft performance |
|
|
Takeoff weight: |
|
|
- normal (with full internal fuel, 2xR-60, 1 tn of bombs), kg |
16,400 |
|
- maximum (with full internal fuel, 4 tn of bombs), kg |
19,430 |
|
Maximum internal fuel, kg |
3,770 |
|
Maximum ordnance, kg |
4,000 |
|
Service ceiling (without external ordnance or stores), km |
14.2 |
|
Maximum flight speed at sea level (without external ordnance or stores), km/h |
1,400 |
|
Max Mach (external ordnance or stores) |
1.7 |
|
G-limit (operational) |
7 |
|
Maximum flight range (with 1 tn ordnance, 4x PTB-800): |
|
|
- at sea level, km |
1,380 |
|
- at height, km |
2,300 |
|
Takeoff run at maximum takeoff weight, m |
|
|
Landing run at normal landing weight (with braking parachute), m |
950 |
|
Aircraft dimensions: |
|
|
- length, m |
19.02 |
|
- wingspan, m |
10.02 (13.68) |
|
- height, m |
5.12 |
|
Crew |
1 |
|
Powerplant |
|
Number and type of engines |
1 x AL-21F3 |
|
Thrust: |
|
|
- in afterburner, kgf |
112,000 |
|
- at full power, kgf |
8,000 |
|
Avionics |
|
|
1. Attack and navigation system |
|
|
1.1 Onboard computer |
|
|
1.2. On-board digital device |
|
|
1.3. Laser target illuminator and rangefinder |
|
|
1.4. Doppler navigator |
|
|
1.5. Sight tube |
|
|
1.6. Digital mapping system |
|
|
1.7. Television signals switching unit |
|
|
1.8. HUD |
|
|
1.9. Air-to-radar missile guidance with Luch display |
|
|
1.10. Attitude and heading reference system |
|
|
1.11. Short range radio navigation and landing system |
|
|
1.12. Short range radio navigation system |
|
|
1.13. Long range radio navigation system |
|
|
1.14. Air data system |
|
|
1.15. Automatic direction finder |
|
|
1.16. Aircraft responder |
|
|
1.17. Control signal generation equipment |
|
|
1.18. Information input system |
|
|
2. GPS system |
|
|
3. Weapons control system |
|
|
4. Autopilot system |
|
|
5. Radio altimeter |
|
|
6. Communications radio transceiver |
|
|
7. IFF transponder |
|
|
8. Marker radio receiver |
|
|
9. Combat performance monitoring system |
|
|
10. Flight recorder |
|
|
11. Defence |
|
|
11.1. Radar warning receiver |
|
|
11.2. Radio jamming transmitter (in pod) |
|
|
11.3. Infrared and passive jamming device |
|
|
12. Sensors (in pod) |
|
|
13. Kh-25MR missile (pod) guidance system |
|
|
14. Infrared imaging system (in pod) |
|
|
15. Kopyo search and track radar system |
|
|
16. Power supply and CEJ pod |
|
|
17. CEJ blocks for Kh-31A |
|
|
Limits |
|
Airframe limit: |
|
|
- SLL, hours |
2,000 |
|
- service life, years |
20 |
