The upgraded supersonic fighter-bomber Su-22M3 is designed for destruction of ground and surface naval targets in daytime and at night under favourable and adverse weather conditions, as well as for air combat and comprehensive reconnaissance missions
| Armaments | |
| 1. Guns | Two 30mm guns, with 80 rds each |
| 2. Guided air-to-surface missiles |
Kh-23M, Kh-25MR (ML, MP), Kh-29L, Kh-28 |
| 3. Guided air-to-air missiles | R-60 (R-60M) |
| 4. Unguided missiles |
S-5, S-8, S-24, S-25 |
| 5. Bombs, calibre, kg | 100, 250, 500 |
| 6. Cluster bombs |
RBK-100 RBK-250 RBK-500 |
| 7. Incendiary bombs | ZB-500 |
| 8. Small-size cargo pods | KMGU |
| 9. External fuel tanks |
PTB-800 (840 l), PTB-1150 (1160 l) |
| 10. Suspension points | 10 |
| Aircraft performance | |
| Takeoff weight: | |
| - normal (without external ordnance or stores, with full integral tankage), kg | 15,590 |
| - maximum, kg | 19,640 |
| 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 | 1,350 |
| Maximum flight speed at high altitude (without external ordnance or stores), km/h | 1,900 |
| g limit (operational) | 7 |
| Maximum flight range (with external tanks and 1 tn ordnance): | |
| - at sea level, km | 1,300 |
| - at height, km | 2,100 |
| Takeoff run at maximum takeoff weight, m | 1,600 |
| Landing run at normal landing weight (with braking parachute), m | 950 |
| Aircraft dimensions: | |
| - length, m | 18.91 |
| - wingspan, m | 10.02 (13.68) |
| - height, m | 5.01 |
| Crew | 1 |
| Powerplant | |
| Number and type of engines | 1 x R-29BS-300 |
| Thrust: | |
| - in afterburner, kgf | 11,500 |
| - in full power, kgf | 800 |
| Avionics | |
| 1. Navigation and flight equipment | |
| 1.1.Navigation | |
| 1.1.1. Attitude and heading reference system | |
| 1.1.2. Doppler navigator | |
| 1.1.3. Short range radio navigation and landing system | |
| 1.2.Automatic direction finder | |
| 1.3. Radio altimeter | |
| 1.4. Air data system | |
| 1.5. Angle-of-attack and g-load indicator | |
| 1.6. Autopilot system | |
| 2. Aiming equipment | |
| 2.1. Aircraft gun bombsight | |
| 2.2. Laser rangefinder and target illuminator | |
| 2.3. Control equipment for X-23M rockets (in pod) | |
| 2.4. Air-to-surface missile guidance set | |
| 3. Radio equipment | |
| 3.1. Communications transceiver | |
| 3.2. IFF transponder | |
| 3.3. Aircraft responder | |
| 4. Defence | |
| 4.1. Radar warning receiver | |
| 4.2. Radio jamming transmitter (in pod) | |
| 4.3. Passive jamming device | |
| 5. Sensors (in pod) | |
| 6. GPS system | |
| Limits | |
| Airframe limit: | |
| - SLL, hours | 2,000 |
| - service life, years | 20 |
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