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]
Su-57E · Length
Single sourceConfiguration
| Specification | Sukhoi Su-30MKM | Sukhoi Su-57 |
|---|---|---|
| Type | Air superiority fighter , Multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | Russia[source] | Russia[source] |
| Designer | Sukhoi[source] | Sukhoi[source] |
| Built by | Irkut Corporation[source] | Komsomolsk-on-Amur Aircraft Plant |
20.1 m (65 ft 11 in)[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; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; Su-30MKM · / M 2.0 at high altitude
Single source2,120 km/h (1,320 mph, 1,140 kn) / M 2.0 at high altitude[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceMach 2.0, 2,135 km/h (1,153 kn; 1,327 mph) at high altitude Mach 1.1, 1,350 km/h (729 kn; 839 mph) at sea level[source]
Ferry; 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]
Ferry; Su-57E · with 2 outboard fuel tanks
Single sourceSu-57E · subsonic
Single sourceSu-57E · Combat range
Single source1,250 km (780 mi, 670 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]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceSu-57E · with afterburner
Single source2 × Saturn AL-41F-1 afterburning turbofan , 88.3 kN (19,900 lbf) thrust each dry, 142.2 kN (32,000 lbf) with afterburner, 147.1 kN (33,100 lbf) in emergency power[source]
Su-30MKM · (59,000 ft/min) +
Single source300 m/s (59,000 ft/min) +[source]
Su-57E · Hardpoints: 12 hardpoints (6 × internal, 6 × external) with a capacity of maximum payload
Single sourceHardpoints: 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In production[source] |
|---|
| Primary user | Royal Malaysian Air Force[source] | — |
|---|
| Number built | 18[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Introduction date | 2007[source] | 2020[source] |
|---|
| First flight | August 2003 ( 2003-08 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Sukhoi Su-30 Sukhoi Su-30MKI[source] | — |
|---|
| g limits | + 9g[source] | +9.0[source] |
|---|
| Wing loading | 401 kg/m 2 (82 lb/sq ft)[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | 0.96[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[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 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Rockets | 4 × B-8 rocket pods for 80 × S-8 rockets 4 × B-13 rocket pods for 20 × S-13 rockets[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 : R-77 M R-74M2 R-37 (missile) Air-to-surface missiles : 4 × Kh-38 M 4 × Kh-69 S-71K Kovyor Anti-ship missiles : 2 × Kh-35 U 2 × Kh-31 Anti-radiation missiles : 4 × Kh-58 UShK[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] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Manufacturer | — | United Aircraft Corporation[source] |
|---|
| Primary users | — | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Manufactured | — | 2019–present[source] |
|---|
| Variant | — | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Fuel capacity | — | 9,700 kg (21,385 lb) internal, 12,900 kg (28,440 lb) with 2× PTB-2000 2,000 L (528 US gal) drop tanks[source] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[source] |
|---|
Gross; Su-57E · normal takeoff weight
Single sourceMaximum take-off; Su-57E · Max takeoff weight
Single source18,500 kg (40,786 lb)[source]
26,700 kg (58,863 lb) normal takeoff weight, 29,800 kg (65,700 lb) at full load[source]
34,000 kg (74,957 lb)[source]
Su-57E · supersonic
Single source