In numbers Through the lens Video
NATO reporting name: Flanker C
The Su-30MK is a two-seat multirole Su-27SK derivative powered by two AL-31F 12.500 kgf engines and featuring uprated avionics and an expanded air-to-air and air-to-surface weapons suite including air-to-surface precision-guided munitions.
The aircraft has an in-flight refuelling capability.
The first production aircraft completed its maiden flight on 19 May 1999. The Su-30MK has been in production with the KnAAPO since 1999.
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY |
Russia
|
| TYPE | Multipurpose fighter |
| CREW | 2 |
| POWER-PLANT | Two turbofan engines ΝPO Saturn Lyl'ka AL-31F |
| Thrust, kgf | 2x12.800 |
| DIMENSIONS | |
| Length, m | 21,90 |
| Height, m | 6,40 |
| Wing span, m | 14,70 |
| Wing area, m2 | 62,00 |
| WEIGHT | |
| Maximum take-off, kg | 34.500 |
| Normal take-off, kg | 24.900 |
| Empty aircraft, kg | - |
| Internal fuel, kg | 9.640 (under normal conditions 5.270) |
| Warload, kg | 8.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude), km/h | 2.175 |
| Maximum speed in low height, km/h | 1.350 |
| Service ceiling, m | 19.800 |
| Rate of climb, m/min | - |
| Range, km | 3.000 |
| Range with an aerial refueling, km | 5.200 |
| Maximum overload, g | - |
| ARMAMENT | 1x30 mm cannon GSh-301 with 150 rounds. Number external hardpoints: 12. Transportation of weapons: 6 Air-to-air missile R-27R/ER/T/ET, R-73 and R-77 (RVV-AE). Anti-ship missile Kh-29T/L, Kh-25ML, Kh-31A/P, Kh-59M and S-25L bombs KAB-500KR/L/D, free fall bombs 100 - 500 kg, cluster bombs, ECM pods. |