FORCETALLY
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At a glance
Measured figures
Length
Single source14.25 m (46 ft 9 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | FMA IA 58 Pucará | Sukhoi Su-57 |
|---|---|---|
| Type | Counter-insurgency aircraft[source] | Stealth multirole fighter[source] |
| National origin | Argentina[source] | Russia[source] |
| Manufacturer | Fábrica Militar de Aviones[source] | United Aircraft Corporation[source] |
| Status | In service[source] | In production |
20.1 m (65 ft 11 in)[source]
Cruise; at 6,000 ft (1,800 m) (econ cruise)
Single sourceMaximum; at 3,000 m (9,800 ft)
Single source500 km/h (310 mph, 270 kn) at 3,000 m (9,800 ft)[source]
430 km/h (270 mph, 230 kn) at 6,000 ft (1,800 m) (econ cruise)[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceFerry; max internal and external fuel
Single source3,710 km (2,310 mi, 2,000 nmi) max internal and external fuel[source]
2 × Turbomeca Astazou XVIG turboprop each
Single source2 × Turbomeca Astazou XVIG turboprop, 729 kW (978 hp) each[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]
3,500 ft/min
Single source18 m/s (3,500 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.
| Primary users | Argentine Air Force Sri Lanka Air Force (historical) Uruguayan Air Force (historical)[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | 110[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 1974–1993[source] | 2019–present[source] |
|---|
| Introduction date | May 1975[source] | 2020[source] |
|---|
| First flight | 20 August 1969[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Aspect ratio | 6.9:1[source] | — |
|---|
| Airfoil | NACA 64 2 A215 at root, NACA64 1 at tip[source] | — |
|---|
| Fuel capacity | 1,280 L (280 imp gal; 340 US gal) internal, up to 1,736 L (382 imp gal; 459 US gal) in external tanks[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] |
|---|
| Stall speed | 143 km/h (89 mph, 77 kn) (flaps and undercarriage down)[source] | — |
|---|
| Never exceed speed | 750 km/h (470 mph, 400 kn)[source] | — |
|---|
| g limits | +6/-3 g[source] | +9.0[source] |
|---|
| Guns | 2× 20 mm Hispano-Suiza HS.804 autocannons 4× 7.62 mm FN Browning machine guns[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 3 with a capacity of centerline 1,000 kg (2,200 lb), wing pylons 500 kg (1,100 lb), total external stores 1,620 kg (3,570 lb)[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Rockets | ARM-657 Mamboretá pods[source] | — |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Variant | — | Sukhoi/HAL FGFA (cancelled)[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] |
|---|
| 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] |
|---|
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]