FORCETALLY
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At a glance
Measured figures
Gross; Gross weight
Single source6,100 lb (2,767 kg)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceGross; 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]
Cruise; at maximum continuous power
Single sourceCruise; combat cruise
Single sourceMaximum; at take-off power, 5,000 ft (1,524 m) altitude, 6,000 lb (2,722 kg) gross weight
Single source148 kn (170 mph, 274 km/h) at take-off power, 5,000 ft (1,524 m) altitude, 6,000 lb (2,722 kg) gross weight[source]
77 kn (88 mph, 142 km/h) at maximum continuous power, 129 kn (239 km/h) combat cruise[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceRange
Single source360 nmi (420 mi, 680 km)[source]
1 × Garrett TPE-331-1-101F turboprop engine
Single source1 × Garrett TPE-331-1-101F turboprop engine, 650 hp (480 kW)[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 · Service ceiling
Single source18,800 m (61,700 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.
Configuration
| Specification | Fairchild AU-23 Peacemaker | Sukhoi Su-57 |
|---|---|---|
| Type | Armed gunship, counter-insurgency, utility transport[source] | Stealth multirole fighter[source] |
| Manufacturer | Fairchild Aircraft[source] | United Aircraft Corporation[source] |
| Primary users | United States Air Force Royal Thai Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
| Number built | 35[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
| First flight | 1971[source] | 29 January 2010 ( 2010-01-29 )[source] |
| Developed from | Pilatus PC-6 Porter[source] | — |
| Capacity | 5 troops or 6 passengers or 1 litter patient, 3 ambulatory patients with 1 medical attendant[source] | — |
| Endurance | 4.84[source] | — |
| National origin | United States[source] | Russia[source] |
| Designer | — | Sukhoi[source] |
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
| Status | — | In production[source] |
| Manufactured | — | 2019–present[source] |
| Introduction date | — | 2020[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] |
| Guns | — | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[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] |
| g limits | — | +9.0[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] |
| Missiles | — | 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-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[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]