The upgraded supersonic fighter-bomber Su-22M4 is designed for destruction of ground and naval surface targets in daytime and at night under favourable and adverse weather conditions, comprehensive reconnaissance and air-to-air "dogfight" combat.
| Armaments | |
| 1. Guns | Two 30mm guns, with 80 rds each |
| 2. Guided air-to-surface missiles |
Kh-58UE, Kh-25ML (MR, MP letter A), Kh-29T (L), S-25L, Kh-31A |
| 3. Guided bomb units | KAB-500KR |
| 4. Guided air-to-air missiles | R-60 (R-60M) |
| 5. Unguided missiles |
S-5, S-24, S-25 |
| 6. Bombs, calibre, kg | 100, 250, 500 |
| 7. Cluster bombs | RBK-500 |
| 8. Incendiary bombs | ZB-500 |
| 9. Small-size cargo pods | KMGU-2 |
| 10. Suspended guns (pivoting to shoot back and forth) | SPPU |
| 11. External fuel tanks |
PTB-800 (840 l), PTB-1,150 (1,160 l) |
| 12. Suspension points | 10 |
| 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 |
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