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At a glance
Measured figures
Mirage 5F · Length
Single source15.55 m (51 ft 0 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Dassault Mirage 5 | Sukhoi Su-57 |
|---|---|---|
| Type | Attack aircraft Fighter-bomber[source] | Stealth multirole fighter[source] |
| National origin | France[source] | Russia[source] |
| Manufacturer | Dassault Aviation[source] | United Aircraft Corporation[source] |
| Status | Active[source] | In production |
20.1 m (65 ft 11 in)[source]
Cruise; Mirage 5F · Cruise speed
Single sourceMaximum; Mirage 5F · at 12,000 m (39,000 ft)
Single source2,350 km/h (1,460 mph, 1,270 kn) at 12,000 m (39,000 ft)[source]
956 km/h (594 mph, 516 kn)[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceFerry; Mirage 5F · Ferry range
Single source4,000 km (2,500 mi, 2,200 nmi)[source]
Mirage 5F · 1 × SNECMA Atar 9C afterburning turbojet thrust dry
Single sourceMirage 5F · with afterburner
Single source1 × SNECMA Atar 9C afterburning turbojet , 41.97 kN (9,440 lbf) thrust dry, 60.8 kN (13,700 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceMirage 5F · Bombs of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks
Single sourceBombs: 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks[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 | French Air Force (historical) Belgian Air Force (historical) Egyptian Air Force (historical) Pakistan Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | 582[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| First flight | 19 May 1967[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Dassault Mirage III[source] | — |
|---|
| Variant | IAI Nesher[source] | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Developed into | IAI Kfir .[source] | — |
|---|
| Guns | 2 × 30 mm (1.18 in) DEFA 552 cannons with 125 rounds per gun[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Wing loading | 391 kg/m 2 (80 lb/sq ft)[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Rockets | 2 × Matra JL-100 drop tank/rocket pack, each with 18 × SNEB 68 mm rockets and 66 US gallons (250 liters) of fuel[source] | — |
|---|
| Missiles | 2 × AIM-9 Sidewinder OR Matra R550 Magic[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 | 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Hardpoints | Bombs: 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Manufactured | — | 2019–present[source] |
|---|
| Introduction date | — | 2020[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] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[source] |
|---|
| g limits | — | +9.0[source] |
|---|
| Thrust/weight | — | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Reported operators |
| — |
|---|
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]