Credit
Anna Zvereva from Tallinn, Estonia · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Su-35S · Length
Single source21.9 m (71 ft 10 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Sukhoi Su-35 | Sukhoi Su-57 |
|---|---|---|
| Type | Multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | Soviet Union ( Russia since 1991)[source] | Russia[source] |
| Manufacturer | United Aircraft Corporation (for Su-35S)[source] | United Aircraft Corporation[source] |
| Designer | Sukhoi Design Bureau[source] | Sukhoi |
20.1 m (65 ft 11 in)[source]
Empty; Su-35S · Empty weight
Single sourceGross; Su-35S · with 50% internal fuel
Single sourceMaximum take-off; Su-35S · Max takeoff weight
Single source19,000 kg (41,888 lb)[source]
25,300 kg (55,777 lb) with 50% internal fuel[source]
34,500 kg (76,059 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceCruise; Su-35S · / Mach 1.1 + supercruise at medium altitude
Single sourceMaximum; Su-35S · at altitude
Single source2,400 km/h (1,490 mph, 1,290 kn) at altitude[source]
1,170 km/h (730 mph, 630 kn) / Mach 1.1 + supercruise at medium altitude[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceFerry; Su-35S · with 2 external fuel tanks
Single sourceSu-35S · at altitude 1,580 km (982 mi) at sea level
Single source3,600 km (2,200 mi, 1,900 nmi) at altitude 1,580 km (982 mi) at sea level[source]
4,500 km (2,800 mi, 2,400 nmi) with 2 external fuel tanks[source]
Ferry; Su-57E · with 2 outboard fuel tanks
Single sourceSu-57E · subsonic
Single sourceSu-35S · 2 × Saturn AL-41F1S afterburning turbofan engines thrust each dry
Single sourceSu-35S · in emergency power
Single sourceSu-35S · with afterburner
Single source2 × Saturn AL-41F1S afterburning turbofan engines, 86.3 kN (19,400 lbf) thrust each dry, 137.3 kN (30,900 lbf) with afterburner, 142.2 kN (32,000 lbf) in emergency power[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceSu-35S · (55,000 ft/min) +
Single source280 m/s (55,000 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.
| Built by | Sukhoi[source] | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Status | In service[source] | In production[source] |
|---|
| Primary users | Russian Aerospace Forces People's Liberation Army Air Force Algerian Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | Su-27M: 12 Su-35S: 155+[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | Su-27M: 1987–1995 Su-35S: 2007–present[source] | 2019–present[source] |
|---|
| Introduction date | February 2014[source] | 2020[source] |
|---|
| First flight | Su-27M: 28 June 1988 ( 1988-06-28 ) Su-35S: 19 February 2008 ( 2008-02-19 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Sukhoi Su-27[source] | — |
|---|
| Variant | Sukhoi Su-37[source] | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Fuel capacity | 11,500 kg (25,400 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] |
|---|
| Guns | 1 × internal 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of ordnance , with provisions to carry combinations of: Rockets: S-25 air-ground rocket S-13 air-ground rocket Missiles: Air-to-air missiles : 8 × R-27 ER/ET 6 × R-73 E/M 12 × R-77 M/P/T/-1 6 × R-74 2 x R-37 Air-to-surface missiles : 6 × Kh-29 L/TE 3 × 3M-14AE Anti-ship missiles : 3 × 3M-54AE1 6 × Kh-31 A/AD Kh-35 U 5 × Kh-59 MK 1 × P-800 Oniks Anti-radiation missiles : 6 × Kh-31 P/PD 5 × Kh-58 UShE Bombs: 8 × KAB-500KR TV-guided bombs 8 × KAB-500L laser-guided bombs 8 × KAB-500OD guided bombs 8 × KAB-500S-E satellite-guided bombs 3 × KAB-1500KR TV-guided bombs 3 × KAB-1500L laser-guided bombs[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Airfoil | 5%[source] | — |
|---|
| g limits | + 9[source] | +9.0[source] |
|---|
| Wing loading | 408 kg/m 2 (84 lb/sq ft) With 50% fuel 500.8 kg/m 2 (102.6 lb/sq ft) with full internal fuel[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | 1.13 with 50% fuel 0.92 with full internal fuel[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Rockets | S-25 air-ground rocket S-13 air-ground rocket[source] | — |
|---|
| Missiles | Air-to-air missiles : 8 × R-27 ER/ET 6 × R-73 E/M 12 × R-77 M/P/T/-1 6 × R-74 2 x R-37 Air-to-surface missiles : 6 × Kh-29 L/TE 3 × 3M-14AE Anti-ship missiles : 3 × 3M-54AE1 6 × Kh-31 A/AD Kh-35 U 5 × Kh-59 MK 1 × P-800 Oniks Anti-radiation missiles : 6 × Kh-31 P/PD 5 × Kh-58 UShE[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-500KR TV-guided bombs 8 × KAB-500L laser-guided bombs 8 × KAB-500OD guided bombs 8 × KAB-500S-E satellite-guided bombs 3 × KAB-1500KR TV-guided bombs 3 × KAB-1500L laser-guided bombs[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[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]
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]