Credit
MSgt Eric Harris · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Mirage F1 · Length
Single source15.3 m (50 ft 2 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Dassault Mirage F1 | Sukhoi Su-57 |
|---|---|---|
| Type | Fighter aircraft[source] | Stealth multirole fighter[source] |
| National origin | France[source] | Russia[source] |
| Manufacturer | Dassault Aviation[source] | United Aircraft Corporation[source] |
| Status | In limited service[source] | In production |
20.1 m (65 ft 11 in)[source]
Empty; Mirage F1 · Empty weight
Single sourceGross; Mirage F1 · clean take-off weight
Single sourceMaximum take-off; Mirage F1 · Max takeoff weight
Single source7,400 kg (16,314 lb)[source]
10,900 kg (24,030 lb) (clean take-off weight)[source]
16,200 kg (35,715 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; Mirage F1 · at 11,000 m (36,000 ft)
Single source2,338 km/h (1,453 mph, 1,262 kn) at 11,000 m (36,000 ft)[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]
Ferry; Mirage F1 · with maximum external fuel
Single source3,300 km (2,100 mi, 1,800 nmi) with maximum external fuel[source]
Mirage F1 · 1 × SNECMA Atar 9K-50 afterburning turbojet engine thrust dry
Single sourceMirage F1 · with afterburner
Single source1 × SNECMA Atar 9K-50 afterburning turbojet engine, 49.03 kN (11,020 lbf) thrust dry, 70.6 kN (15,900 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceMirage F1 · combat air patrol, with 2 × Super 530 missiles and centreline drop tank
Single source2 hr 15 min (combat air patrol, with 2 × Super 530 missiles and centreline drop tank)[source]
Mirage F1 · 47,800 ft/min
Single source243 m/s (47,800 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 | French Air Force (historical) Iraqi Air Force (historical) Hellenic Air Force (historical) Spanish Air Force (historical)[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | 726[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 1966–1992[source] | 2019–present[source] |
|---|
| Introduction date | 1973 ( 1973 )[source] | 2020[source] |
|---|
| First flight | 23 December 1966 ( 1966-12-23 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Dassault Mirage III[source] | — |
|---|
| Guns | 2× 30 mm (1.18 in) DEFA 553 cannons with 150 rounds per gun[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 1 centreline pylon, four underwing and two wingtip pylons with a capacity of 6,300 kg (13,900 lb) (practical maximum load 4,000 kg (8,800 lb)), with provisions to carry combinations of: Rockets: 8× Matra rocket pods with 18× SNEB 68 mm rockets each Bombs: various Other: 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] |
|---|
| Thrust/weight | 0.66[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Rockets | 8× Matra rocket pods with 18× SNEB 68 mm rockets each[source] | — |
|---|
| Bombs | various[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Other | reconnaissance pods or Drop tanks[source] | — |
|---|
| Missiles | 2× AIM-9 Sidewinders OR Matra R550 Magics on wingtip pylons, 2× R.530 or Super 530 Fs underwing, 1× AM-39 Exocet anti-ship missile, 2× AS-30L laser-guided missiles[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] |
|---|
| Alternative designation | Mirage F1[source] | — |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[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] |
|---|
| 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] |
|---|
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]
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]