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At a glance
Measured figures
MiG-35 · Length
Single source17.3 m (56 ft 9 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Mikoyan MiG-35 | Sukhoi Su-57 |
|---|---|---|
| Type | Multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | Russia[source] | Russia[source] |
| Manufacturer | United Aircraft Corporation[source] | United Aircraft Corporation[source] |
| Designer | Mikoyan[source] | Sukhoi[source] |
20.1 m (65 ft 11 in)[source]
Empty; MiG-35 · Empty weight
Single sourceGross; MiG-35 · Gross weight
Single sourceMaximum take-off; MiG-35 · Max takeoff weight
Single source11,000 kg (24,251 lb)[source]
17,500 kg (38,581 lb)[source]
24,500 kg (54,013 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceCruise; MiG-35 · Cruise speed
Single sourceMaximum; MiG-35 · at altitude
Single source2,100 km/h (1,300 mph, 1,100 kn) at altitude[source]
804.7 km/h (500.0 mph, 434.5 kn)[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceFerry; MiG-35 · With 3 external fuel tanks
Single sourceMiG-35 · Range
Single source2,100 km (1,300 mi, 1,100 nmi)[source]
3,000 km (1,900 mi, 1,600 nmi) With 3 external fuel tanks[source]
Ferry; Su-57E · with 2 outboard fuel tanks
Single sourceSu-57E · subsonic
Single sourceMiG-35 · 2 × Klimov RD-33MK afterburning turbofan engines thrust each dry
Single sourceMiG-35 · with afterburner
Single source2 × Klimov RD-33MK afterburning turbofan engines, 52 kN (12,000 lbf) thrust each dry, 88.2 kN (19,800 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceMiG-35 · 65,000 ft/min
Single source330 m/s (65,000 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 | Russian Aerospace Forces[source] | — |
|---|
| Number built | 6+ serial and 2 to 8 test aircraft[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 2016–2024[source] | 2019–present[source] |
|---|
| Introduction date | 17 June 2019[source] | 2020[source] |
|---|
| First flight | December 2016 ( 2016-12 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Mikoyan MiG-29M Mikoyan MiG-29K[source] | — |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 100 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 9 hardpoints with a capacity of up to 6,500 kg , with provisions to carry combinations of: Rockets: S-8 S-13 S-25 L (LD) laser-guided variant S-25 -O with fragmentation warhead and radio proximity fuze S-24 Missiles: Air-to-air missiles : R-73 R-77 Air-to-surface missiles : Kh-25 MAE Kh-29L/TE Kh-38ME Kh-38 Grom-E1 Anti-radiation missiles : 4 × Kh-31 PD Anti-ship missiles : 4 × Kh-31 AD Bombs: KAB-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500S-E GLONASS guided bomb[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Max landing weight | 16,800 kg (37,000 lb)[source] | — |
|---|
| g limits | + 9 - 3[source] | +9.0[source] |
|---|
| Rockets | S-8 S-13 S-25 L (LD) laser-guided variant S-25 -O with fragmentation warhead and radio proximity fuze S-24[source] | — |
|---|
| Missiles | Air-to-air missiles : R-73 R-77 Air-to-surface missiles : Kh-25 MAE Kh-29L/TE Kh-38ME Kh-38 Grom-E1 Anti-radiation missiles : 4 × Kh-31 PD Anti-ship missiles : 4 × Kh-31 AD[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-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500S-E GLONASS guided bomb[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Primary users | — | Russian Aerospace Forces Algerian Air Force[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] |
|---|
| Wing loading | — | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | — | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[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 source3,500 km (2,200 mi, 1,900 nmi) subsonic 1,500 km (932 mi; 810 nmi) supersonic[source]
4,500 km (2,800 mi, 2,400 nmi) with 2 outboard fuel tanks[source]
Su-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]