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At a glance
Measured figures
Su-30MKK/MK2 · Length
Single source21.9 m (71 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | Sukhoi Su-30MKK | Sukhoi Su-33 |
|---|---|---|
| Type | Multirole strike fighter[source] | Carrier-based air superiority fighter with multirole capabilities[source] |
| National origin | Russia[source] | Soviet Union Russia[source] |
| Designer | Sukhoi[source] | — |
| Status | In service[source] | In service[source] |
21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
Maximum; Su-30MKK/MK2 · at high altitude, or
Single sourceMaximum; Su-30MKK/MK2 · at low altitude
Single source2,120 km/h (1,320 mph, 1,140 kn) at high altitude, or 1,400 kilometres per hour (870 mph) at low altitude[source]
Maximum; at 10,000 m (33,000 ft)
Single source2,300 km/h (1,430 mph, 1,240 kn) at 10,000 m (33,000 ft)[source]
Su-30MKK/MK2 · with 24,900 kilograms (54,900 lb) take-off weight at cruise altitude, or
Single sourceSu-30MKK/MK2 · with the same TOW at low altitude
Single source3,000 km (1,900 mi, 1,600 nmi) with 24,900 kilograms (54,900 lb) take-off weight at cruise altitude, or 1,270 kilometres (790 mi) with the same TOW at low altitude[source]
Range
Single source3,000 km (1,900 mi, 1,600 nmi)[source]
Su-30MKK/MK2 · 2 × Lyulka AL-31F afterburning turbofan engines with afterburner
Single source2 × Lyulka AL-31F afterburning turbofan engines, 122.6 kN (27,600 lbf) with afterburner[source]
2 × Saturn AL-31F3 afterburning turbofan engines thrust each dry
Single sourcewith afterburner
Single source2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 125.5 kN (28,200 lbf) with afterburner[source]
Wing area
Single source67.84 m 2 (730.2 sq ft)[source]
48,400 ft/min
Single source246 m/s (48,400 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | People's Liberation Army Air Force Vietnam People's Air Force Venezuelan Air Force[source] | — |
|---|
| Manufactured | 2000–2016[source] | 1987–1999[source] |
|---|
| Introduction date | December 2000[source] | 31 August 1998 (official)[source] |
|---|
| Developed from | Sukhoi Su-30[source] | Sukhoi Su-27[source] |
|---|
| Fuel capacity | 9,640 kg (21,250 lb) internal[source] | 9,500 kg (20,900 lb) internal[source] |
|---|
| g limits | + 9g[source] | + 8[source] |
|---|
| Thrust/weight | 0.83[source] |
|---|
| Take-off run | 550 m (1,804 ft)[source] | — |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Rockets | various unguided rockets[source] | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Missiles | Air-to-air missiles : R-73 E R-27 R-77 Air-to-surface missiles : Kh-29 T Kh-59 ME Anti-radiation missiles : Kh-31 P[source] | Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P[source] |
|---|
| Bombs | KAB-500L laser-guided bomb KAB-1500L laser-guided bomb various unguided bombs[source] | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Manufacturer | — | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
|---|
| Primary user | — | Russian Navy[source] |
|---|
| Number built | — | 24 built total[source] |
|---|
| First flight | — | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Variant | — | Shenyang J-15[source] |
|---|
| Hardpoints | — | 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P Bombs: RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| Wing loading | — | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Landing speed | — | 240 km/h (150 mph; 130 kn)[source] |
|---|
Maximum take-off; Max takeoff weight