FORCETALLY
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At a glance
Measured figures
Length
Single source5.80 m (19 ft 0 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Nieuport 21 | Sukhoi Su-57 |
|---|---|---|
| Type | Fighter[source] | Stealth multirole fighter[source] |
| Manufacturer | Nieuport[source] | United Aircraft Corporation[source] |
| Designer | Gustave Delage[source] | Sukhoi[source] |
| Primary users | Aéronautique Militaire Imperial Russian Air Service US Army Air Service[source] | Russian Aerospace Forces Algerian Air Force |
20.1 m (65 ft 11 in)[source]
Su-57E · Wingspan
Single source14.1 m (46 ft 3 in)[source]
Maximum; Maximum speed
Single source150 km/h (93 mph, 81 kn)[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceMach 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]
Range
Single source250 km (160 mi, 130 nmi)[source]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[source]
1 × Le Rhône 9C air-cooled rotary engine
Single source1 × Le Rhône 9C air-cooled rotary engine , 60 kW (80 hp)[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 · 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.
| Introduction date | 1 August 1916[source] | 2020[source] |
|---|
| First flight | June 1916[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Retired | 1920s[source] | — |
|---|
| Developed from | Nieuport 17[source] | — |
|---|
| Upper wingspan | 8.16 m (26 ft 9 in)[source] | — |
|---|
| Upper Chord | 1.233 m (4 ft 0.5 in)[source] | — |
|---|
| Wing Sweep | 3° 20'[source] | — |
|---|
| Lower wingspan | 7.80 m (25 ft 7 in)[source] | — |
|---|
| Lower Chord | 720 m (2,360 ft)[source] | — |
|---|
| Airfoil | — |
|---|
| Undercarriage track | 1.60 m (5 ft 3 in)[source] | — |
|---|
| Propellers | 2-bladed Levasseur 450 or Régy 310 fixed pitch wooden propeller, 2.50 m (8 ft 2 in) diameter[source] | — |
|---|
| Time to altitude | 8.45 minutes 2,000 m (6,600 ft) 15.7 minutes 3,000 m (9,800 ft)[source] | — |
|---|
| Guns | 1 x .303 in (7.7 mm) Vickers machine gun[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| National origin | France[source] | Russia[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Status | — | In production[source] |
|---|
| Number built | — | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | — | 2019–present[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] |
|---|
| 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] |
|---|
Gross; Su-57E · normal takeoff weight
Single sourceMaximum take-off; Su-57E · Max takeoff weight
Single source