Credit
Rob Schleiffert from Holland · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Mirage 2000D/N · Length
Single source14.55 m (47 ft 9 in)[source]
Su-57E · Length
Configuration
| Specification | Dassault Mirage 2000N/2000D | Sukhoi Su-57 |
|---|---|---|
| Type | Multirole combat aircraft[source] | Stealth multirole fighter[source] |
| National origin | France[source] | Russia[source] |
| Manufacturer | Dassault Aviation[source] | United Aircraft Corporation[source] |
| Status | Active (2000D only)[source] | In production |
20.1 m (65 ft 11 in)[source]
Empty; Mirage 2000D/N · Empty weight
Single sourceGross; Mirage 2000D/N · Gross weight
Single sourceMaximum take-off; Mirage 2000D/N · Max takeoff weight
Single source7,600 kg (16,755 lb)[source]
10,680 kg (23,545 lb)[source]
17,000 kg (37,479 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; Mirage 2000D/N · Maximum speed
Single source1,728 km/h (1,074 mph, 933 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]
Ferry; Mirage 2000D/N · Ferry range
Single source3,340 km (2,080 mi, 1,800 nmi)[source]
Mirage 2000D/N · 1 × SNECMA M53-P2 afterburning turbofan engine thrust dry
Single sourceMirage 2000D/N · with afterburner
Single source1 × SNECMA M53-P2 afterburning turbofan engine, 64 kN (14,000 lbf) thrust dry, 95.1 kN (21,400 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceMirage 2000D/N · 56,100 ft/min
Single source285 m/s (56,100 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 user | French Air and Space Force[source] | — |
|---|
| Number built | 161 (75 Mirage 2000N and 86 Mirage 2000D)[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| First flight | 3 February 1986[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Retired | 2018 (2000N)[source] | — |
|---|
| Developed from | Mirage 2000[source] | — |
|---|
| Wing loading | 410 kg/m 2 (84 lb/sq ft)[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | * Propulsive efficiency: 0.91 (non dimensional)[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Rockets | Up to 4× Matra SNEB 68-mm 18-round rocket pods on the four underwing hardpoints[source] | — |
|---|
| Missiles | Air-to-air missiles : Up to 4× R550 Magic air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Up to 6× MICA air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Air-to-surface missiles : – Mirage 2000N 1× ASMP medium-range nuclear missile on the centerline pylon Air-to-surface missiles : – Mirage 2000D 1× Apache anti-runway cruise missile on the centerline pylon 1× SCALP EG air-launched cruise missile on the centerline pylon 2× AS-30L laser-guided missiles on the inboard underwing pylons[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] |
|---|
| Air-to-air missiles | Up to 4× R550 Magic air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Up to 6× MICA air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons[source] | — |
|---|
| Air-to-surface missiles | – Mirage 2000N 1× ASMP medium-range nuclear missile on the centerline pylon[source] | — |
|---|
| Bombs | AASM 125, 250, 1000 Kg laser, ISN/GPS, IIR guided bombs. The lighter versions are carried in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 10× GBU-12 227 Kg laser-guided bombs or GBU-49 227 Kg INS/GPS and laser guided bombs, in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 3× GBU-16 454 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-10 907 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-24 907 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-400 400 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-1000 1000 Kg laser-guided bombs on the centerline and inboard wing hardpoints[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Other | ATLIS II laser/electro-optical targeting pod on the front-right fuselage hardpoint PDLCT laser/electro-optical targeting pod on the front-right fuselage hardpoint Damoclès laser targeting pod on the front-right fuselage hardpoint 1× centerline mounted 345-gallon drop tank 2x either 375, 440 or 530 gallon tanks for ferry flight/extended range/loitering time up to 2× 30 mm CC630 gun pods with 600 rounds per pod, one on each inboard wing hardpoint[source] | — |
|---|
| Hardpoints | 4× under-wing, 4× under fuselage, 1× centerline , with provisions to carry combinations of:[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] |
|---|
| Primary users | — | Russian Aerospace Forces Algerian Air Force[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] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[source] |
|---|
| g limits | — | +9.0[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]