The Su-30MK aeroplane has been designed on the platform of the Su-27UB; it is in series production in Komsomolsk-on-Amur and in Irkutsk.
The Su-30MK is a two-seat highly-manoeuvrable fighter designed for air-superiority and strikes at ground and naval surface targets using a variety of guided and unguided ADO, with an option of supporting group actions.
| Aircraft performance | |
| Takeoff weight: | |
| - normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg | 24,900* |
| - maximum, kg | 34,500 |
| - max, kg | 38,800 |
| Maximum landing weight, kg | 23,600 |
| Max landing weight, kg | 30,000 |
| Maximum internal fuel, kg | 9,640 |
| Normal internal fuel, kg | 5,270 |
| Maximum ordnance, kg | 8,000 |
| Service ceiling (without external ordnance and stores), km | 17.3 |
| Maximum flight speed at sea level (without external ordnance and stores), km/h | 1,350 |
| Max Mach (without external ordnance and stores) | 2.00 (1.9**) |
| G-limit (operational) | 9 |
| Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance): | |
| - at sea level, km | 1,270 |
| - at height, km | 3,000 |
| - with one refuelling (at 1.500 kg fuel remaining), km | 5,200 |
| - with two refuellings in flight, km | 8,000 |
| Maximum airborne time (pilot-dependent), hours | 10 |
| Takeoff run at normal takeoff weight, m | 550 |
| Landing run at normal landing weight (with braking parachute), m | 750 |
| Aeroplane dimensions: | |
| - length, m | 21.9 |
| - wingspan, m | 14.7 |
| - height, m | 6.4 |
| Crew | 2 |
| In-flight refuelling system | |
| Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min | 1,100 |
| Powerplant | |
| Number and type of engines | 2 x AL-31F (2 x AL-31FP***) |
| Thrust in afterburner, kgf | 12,500 -2 % |
| Avionics | |
| 1. Fire control system | |
| 1.1. Air-to-air fire control system | |
| 1.1.1. Search and track radar | |
| 1.1.2. IRST and laser rangefinder | |
| 1.1.2.1. Optical search and track station | |
| 1.1.2.2. Helmet-mounted target designator | |
| 1.1.3. Wide-angle HUD | |
| 1.1.4. IFF system interrogator | |
| 1.2. Air-to-surface fire control system | |
| 1.2.1. Coloured multi-purpose LCD indicators | |
| 1.2.2. Onboard digital computer | |
| 1.2.3. GPS satellite-based navigation system | |
| 1.2.4. Weapons control system | |
| 2. Aeroplane remote control system | |
| 3. IFF system transponder | |
| 4. Antenna feed system | |
| 5. Flight navigation system | |
| 5.1. Digital computer | |
| 5.2. Attitude and heading reference system | |
| 5.3. Short-range radiotechnical navigation system | |
| 5.4. GPS system | |
| 5.5. Autopilot system | |
| 5.6. Altitude and speed data processing and display system | |
| 5.7. Air data system | |
| 6. Electronic countermeasure equipment | |
| 6.1. Radar warning receiver with an expansion block | |
| 6.2. Chaff and heat flare dispenser | |
| 6.3. Radio jamming transmitter (in pod) | |
| 7. Communications system | |
| 7.1. VHF and UHF band communications transceiver | |
| 7.2. VHF and UHF band communications transceiver | |
| 7.3. SW band radio communications transceiver | |
| 8. Onboard automatic control system | |
| 8.1. Integrated onboard control and crew warning system | |
| 8.2. Flight information recording equipment | |
| 8.3. Onboard emergency situation warning equipment | |
| 9. Video recording system | |
| 9.1. Onboard video recorder | |
| 9.2. Forward vision video camera | |
| 9.3. Video controller | |
| 10. Aircraft responder | |
| 11. Telecommand homing system | |
| 12. Pod-type IRST and laser rangefinder | |
| Limits | |
| Aircraft limit: | |
| - SLL, hours | 3,000 |
| - to first overhaul, hours | 1,500 |
| - service life, years | 25 |
| Engine and outboard accessory-gearbox life: | |
| - to first overhaul, hours | 500 |
| - service life limit, hours | 1,500 |
**With canard surfaces installed
***With thrust vector control engine installed
| Armaments | |
| 1. Guns | Onboard 30mm gun with 150 rds |
| 2. Guided air-to-air missiles | R-27R1(ER1) R-27T1(ET1) R-27P(EP) R-73E RVV-AYe |
| 3. Guided air-to-surface missiles | Kh-59ME Kh-31A, Kh-31P Kh-29T(TYe), Kh-29L |
| 4. Guided bomb units | KAB-500KR, KAB-500OD KAB-1500KR, KAB-1500L |
| 5. Air bombs | FAB-500T BETAB-500ShP ODAB-500PM OFAB-250-270 OFAB-100-120 P-50T Incendiary bombs |
| 6. Cluster bombs | RBK-500 SPBE-D |
| 7. Unguided missiles | S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU |
| 8. External fuel tanks | N/a |
| 9. Suspension points | 12 |
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