Credit
US Air Force photo by Staff Sgt. Peter Thompson, via Wikimedia Commons · Public domain in the United States — US Air Force official work · Source ↗ · Modified
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At a glance
Measured figures
Empty; F-35A · Empty weight
Single sourceGross; F-35A · Gross weight
Single sourceMaximum take-off; F-35A · Max takeoff weight
Single source29,300 lb (13,290 kg)[source]
49,540 lb (22,471 kg)[source]
65,918 lb (29,900 kg)[source]
13.300 kg[source]F-35A · LeergewichtSource text · numeric interpretation needs review
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; F-35A · at sea level
Single sourceMaximum; F-35A · Mach 1.6 at high altitude ( Mach 1.06
Single sourceMach 1.6 at high altitude (1,228 mph / 1,976 km/h) Mach 1.06, 700 knots (806 mph; 1,296 km/h) at sea level[source]
Mach 1,6 (rund 1.930 km/h)[source]F-35A · HöchstgeschwindigkeitSource text · numeric interpretation needs review
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceF-35A · air-to-air configuration on internal fuel
Single sourceF-35A · interdiction mission (air-to-surface) on internal fuel
Single source669 nmi (770 mi, 1,239 km) interdiction mission (air-to-surface) on internal fuel 760 nmi (870 mi; 1,410 km), air-to-air configuration on internal fuel[source]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[source]
F-35A · 1 × Pratt & Whitney F135-PW-100 afterburning turbofan thrust dry
Single sourceF-35A · with afterburner
Single source1 × Pratt & Whitney F135-PW-100 afterburning turbofan , 28,000 lbf (120 kN) thrust dry, 43,000 lbf (190 kN) with afterburner[source]
178 kN[source]F-35A · Maximaler Schub
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceSu-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.
Configuration
| Specification | F-35A | Sukhoi Su-57 |
|---|---|---|
| Fuel capacity | 18,250 lb (8,278 kg) internal[source] 8.278 kg[source]F-35A · KraftstoffkapazitätSource text · numeric interpretation needs review | 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 × 25 mm GAU-22/A 4-barrel rotary cannon , 180 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
| Hardpoints | 4 × internal stations, 6 × external stations on wings with a capacity of 5,700 pounds (2,600 kg) internal, 15,000 pounds (6,800 kg) external, 18,000 pounds (8,200 kg) total weapons payload, with provisions to carry combinations of: Missiles: Air-to-air missiles : AIM-9X Sidewinder AIM-120 AMRAAM AIM-132 ASRAAM AIM-260 JATM (being integrated) MBDA Meteor (Block 4, for F-35B, not before 2027) Air-to-surface missiles : AGM-88G AARGM-ER (Block 4) AGM-158 JASSM SPEAR 3 (Block 4, in development, integration contracted) AGM-88J Stand-in Attack Weapon (SiAW) Anti-ship missiles : AGM-158C LRASM (being integrated) Joint Strike Missile (being integrated) Hypersonic Attack Cruise Missile (Australia; after 2027) Bombs: Joint Direct Attack Munition Paveway Precision-guided glide bomb : AGM-154 JSOW GBU-39 Small Diameter Bomb GBU-53/B StormBreaker B61 mod 12 nuclear bomb[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
| Aspect ratio | 2.66[source] | — |
| g limits | +9.0[source] | +9.0[source] |
| Wing loading | 107.7 lb/sq ft (526 kg/m 2 ) at gross weight[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
| Thrust/weight | 0.87 at gross weight (1.07 at loaded weight with 50% internal fuel)[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
| Missiles | Air-to-air missiles : AIM-9X Sidewinder AIM-120 AMRAAM AIM-132 ASRAAM AIM-260 JATM (being integrated) MBDA Meteor (Block 4, for F-35B, not before 2027) Air-to-surface missiles : AGM-88G AARGM-ER (Block 4) AGM-158 JASSM SPEAR 3 (Block 4, in development, integration contracted) AGM-88J Stand-in Attack Weapon (SiAW) Anti-ship missiles : AGM-158C LRASM (being integrated) Joint Strike Missile (being integrated) Hypersonic Attack Cruise Missile (Australia; after 2027)[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 | Joint Direct Attack Munition Paveway Precision-guided glide bomb : AGM-154 JSOW GBU-39 Small Diameter Bomb GBU-53/B StormBreaker B61 mod 12 nuclear bomb[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
| Manufacturer | Lockheed Martin[source]F-35A · Hersteller | United Aircraft Corporation[source] |
| Tailplane span | 6,86 m[source]F-35A · Spannweite Höhenleitwerk | — |
| Powerplant | Pratt & Whitney F135-PW-100[source]F-35A · Triebwerke | — |
| Maximum load factor | 9 g[source]F-35A · Maximale Belastung | — |
| Type | — | Stealth multirole fighter[source] |
| National origin | — | Russia[source] |
| Designer | — | Sukhoi[source] |
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
| Status | — | In production[source] |
| Primary users | — | Russian Aerospace Forces Algerian Air Force[source] |
| Number built | — | 44+ as of 2026 (including 10 test aircraft)[source] |
| Manufactured | — | 2019–present[source] |
| Introduction date | — | 2020[source] |
| First flight | — | 29 January 2010 ( 2010-01-29 )[source] |
| Variant | — | Sukhoi/HAL FGFA (cancelled)[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 · 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]