Credit
Shahram Sharifi · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Su-57E · Length
Single source20.1 m (65 ft 11 in)[source]
Configuration
| Specification | HESA Saeqeh | Sukhoi Su-57 |
|---|---|---|
| Type | Light fighter[source] | Stealth multirole fighter[source] |
| Manufacturer | Iran Aircraft Manufacturing Industrial Company (HESA)[source] | United Aircraft Corporation[source] |
| Status | Production completed[source] | In production[source] |
| Primary user | Islamic Republic of Iran Air Force[source] | — |
Su-57E · Wingspan
Single source14.1 m (46 ft 3 in)[source]
Su-57E · Height
Single source4.6 m (15 ft 1 in)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceGross; 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]
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]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[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 · Wing area
Single source78.8 m 2 (848 sq ft)[source]
Su-57E · Service ceiling
Single source18,800 m (61,700 ft)[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.
| Number built |
|---|
12[source] |
44+ as of 2026 (including 10 test aircraft)[source] |
| Introduction date | 22 September 2007[source] | 2020[source] |
|---|
| First flight | July 2004[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Northrop F-5 HESA Azarakhsh[source] | — |
|---|
| Developed into | HESA Kowsar[source] | — |
|---|
| Powerplant | 2 × Upgraded Iranian-built General Electric J85 afterburning turbojet engines (with technology from the Pratt & Whitney TF30 )[source] | — |
|---|
| National origin | — | Russia[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] |
|---|
| 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] |
|---|
| 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] |
|---|