FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Su-30MKM · Length
Single source21.935 m (72 ft 0 in)[source]
Length
Single sourceConfiguration
| Specification | Sukhoi Su-30MKM | Sukhoi Su-33 |
|---|---|---|
| Type | Air superiority fighter , Multirole fighter[source] | Carrier-based air superiority fighter with multirole capabilities[source] |
| National origin | Russia[source] | Soviet Union Russia[source] |
| Designer | Sukhoi[source] | — |
| Built by | Irkut Corporation[source] | — |
| Status | In service[source] |
21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
Empty; Su-30MKM · Empty weight
Single sourceGross; Su-30MKM · typical mission weight
Single sourceMaximum take-off; Su-30MKM · Max takeoff weight
Single source18,400 kg (40,565 lb)[source]
26,090 kg (57,519 lb) typical mission weight[source]
38,800 kg (85,539 lb)[source]
Empty; Empty weight
Single sourceGross; Gross weight
Single sourceFerry; Su-30MKM · with two in-flight refuellings
Single sourceSu-30MKM · at high altitude
Single source3,000 km (1,900 mi, 1,600 nmi) at high altitude[source]
8,000 km (5,000 mi, 4,300 nmi) with two in-flight refuellings[source]
Range
Single source3,000 km (1,900 mi, 1,600 nmi)[source]
Su-30MKM · 2 × Lyulka AL-31FP afterburning turbofan engines with afterburner
Single source2 × Lyulka AL-31FP afterburning turbofan engines, 123 kN (28,000 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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Primary user | Royal Malaysian Air Force[source] | Russian Navy[source] |
|---|
| Number built | 18[source] | 24 built total[source] |
|---|
| Introduction date | 2007[source] | 31 August 1998 (official)[source] |
|---|
| First flight | August 2003 ( 2003-08 )[source] | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Developed from | Sukhoi Su-30 Sukhoi Su-30MKI[source] | Sukhoi Su-27[source] |
|---|
| g limits | + 9g[source] | + 8[source] |
|---|
| Wing loading | 401 kg/m 2 (82 lb/sq ft)[source] | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Thrust/weight | 0.96[source] | 0.83[source] |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | 12 hardpoints (2 × wingtip AAM rails, 6 × under-wing pylons, 2 × pylon under-engine nacelles , and 2 × pylons in tandem in the "arch" between the engines. It can be increased to 14 using multiple ejector racks.) with a capacity of up to 8,130 kg (17,920 lb), with provisions to carry combinations of:[source] | 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] |
|---|
| Rockets | 4 × B-8 rocket pods for 80 × S-8 rockets 4 × B-13 rocket pods for 20 × S-13 rockets[source] | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Missiles | Air-to-air missiles : 10 × R-77 6 × R-27ER/ET 2 × R-27R/T 6 × R-73 Air-to-surface missiles : 3 × Kh-59ME 6 × Kh-29T/L Anti-ship missiles : 3 × Kh-59MK 4 × Kh-31A Anti-radiation missiles : 6 × Kh-31P[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 | 8 × KAB-500L laser-guided bombs 3 × KAB-1500L laser-guided bombs 8 × FAB-500T bombs 28 × OFAB-250-270 bombs 32 × OFAB-100-120 bombs 4 × GBU-12 Paveway II laser-guided bomb[source] | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Manufacturer | — | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
|---|
| Manufactured | — | 1987–1999[source] |
|---|
| Variant | — | Shenyang J-15[source] |
|---|
| Fuel capacity | — | 9,500 kg (20,900 lb) internal[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| Landing speed | — | 240 km/h (150 mph; 130 kn)[source] |
|---|
Maximum take-off; Max takeoff weight