FORCETALLY
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At a glance
Measured figures
Su-30MKK/MK2 · Length
Single source21.9 m (71 ft 10 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Sukhoi Su-30MKK | Sukhoi Su-57 |
|---|---|---|
| Type | Multirole strike fighter[source] | Stealth multirole fighter[source] |
| National origin | Russia[source] | Russia[source] |
| Designer | Sukhoi[source] | Sukhoi[source] |
| Status | In service[source] | In production |
20.1 m (65 ft 11 in)[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; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceSu-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]
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-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]
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-57E · Wing area
Single source78.8 m 2 (848 sq ft)[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.
| Primary users | People's Liberation Army Air Force Vietnam People's Air Force Venezuelan Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Manufactured | 2000–2016[source] | 2019–present[source] |
|---|
| Introduction date | December 2000[source] | 2020[source] |
|---|
| Developed from | Sukhoi Su-30[source] | — |
|---|
| Fuel capacity | 9,640 kg (21,250 lb) internal[source] | 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] |
|---|
| g limits | + 9g[source] | +9.0[source] |
|---|
| Thrust/weight | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[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[source] |
|---|
| Rockets | various unguided rockets[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 : 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 | KAB-500L laser-guided bomb KAB-1500L laser-guided bomb various unguided bombs[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] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Number built | — | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| First flight | — | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Variant | — | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Hardpoints | — | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[source] |
|---|
| Wing loading | — | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[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]
Mach 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]
Su-57E · supersonic
Single source