Credit
Srđan Popović · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
J-22 · fuselage length
Single sourceJ-22 · including nose probe
Single sourceConfiguration
| Specification | Soko J-22 Orao | Sukhoi Su-57 |
|---|---|---|
| Type | Attack aircraft Reconnaissance aircraft[source] | Stealth multirole fighter[source] |
| Manufacturer | SOKO[source] | United Aircraft Corporation[source] |
| Designer | VTI - Yugoslavia INCAS - Romania[source] | Sukhoi[source] |
| Status | Active[source] | In production[source] |
13.02 m (42 ft 9 in) (fuselage length); 14.90 m (48 ft 11 in) (including nose probe)[source]
Su-57E · Length
Single source20.1 m (65 ft 11 in)[source]
Empty; J-22 · Empty weight
Single sourceGross; J-22 · clean
Single sourceMaximum take-off; J-22 · Max takeoff weight
Single source5,500 kg (12,125 lb)[source]
8,170 kg (18,012 lb) (clean)[source]
11,080 kg (24,427 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; J-22 · at sea level; Mach 0.96 at 11,000 m (36,000 ft)
Single source1,130 km/h (700 mph, 610 kn) at sea level; Mach 0.96 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; J-22 · (2× 500 L (130 US gal; 110 imp gal) drop tanks)
Single source1,320 km (820 mi, 710 nmi) (2× 500 L (130 US gal; 110 imp gal) drop tanks)[source]
J-22 · (hi-lo-hi profile with 4× BL755 cluster bombs and 1× 1,500 L (400 US gal; 330 imp gal) drop tank)
Single source522 km (324 mi, 282 nmi) (hi-lo-hi profile with 4× BL755 cluster bombs and 1× 1,500 L (400 US gal; 330 imp gal) drop tank)[source]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[source]
J-22 · 2 × Orao/Turbomecanica-built Rolls-Royce Viper Mk 633-47 turbojets thrust each dry
Single sourceJ-22 · with afterburner
Single source2 × Orao/Turbomecanica-built Rolls-Royce Viper Mk 633-47 turbojets , 17.79 kN (4,000 lbf) thrust each dry, 22.24 kN (5,000 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceJ-22 · 17,520 ft/min
Single source89.0 m/s (17,520 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 | Serbian Air Force Yugoslav Air Force (historical) Bosnian Air Force (historical) Republika Srpska Air Force (historical)[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Manufactured | 1974–1992[source] | 2019–present[source] |
|---|
| Introduction date | 1978[source] | 2020[source] |
|---|
| First flight | 31 October 1974[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Variant | IAR-93 Vultur[source] | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Aspect ratio | 3.33:1[source] | — |
|---|
| Airfoil | NACA 65A-008 (modified)[source] | — |
|---|
| Fuel capacity | 3,120 L (820 US gal; 690 imp gal)[source] | 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] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (gear and flaps down)[source] | — |
|---|
| g limits | -4.2 - +8[source] | +9.0[source] |
|---|
| Thrust/weight | 0.44 at gross weight[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Guns | 2× GSh-23L cannons in lower front fuselage, below engine air intakes, with 200 rounds per gun[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 5 (4 underwing and 1 centreline) with a capacity of 500 kg (1,100 lb) wing hardpoints, 800 kg (1,800 lb) fuselage station, 2,800 kg (6,200 lb) total, 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] |
|---|
| Rockets | BRZ-127 rockets, L-57-16MD (UB-16) rocket pods, L-128-04 rocket pods[source] | — |
|---|
| Missiles | AGM-65B Maverick TV guided AGM or Grom-1 AGM (based on Soviet Kh-23 ), VRVZ-200 infrared homing AGM (Only fitted to modernised variants of the J-22, there are TV guided variants of the missile), VRVZ-240 infrared homing AGM (Only fitted to modernised variants of the J-22) R-60MK infrared homing AAM[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 | 50/100/250/500 kg general-purpose bombs , BL755 cluster bombs , PLAB-350 napalm bombs, LVB-250F Laser-guided bomb (based off the FAB-250 bomb, that has been modified with a guidance system, only fitted to modernised variants of the J-22)[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Other | Matra Durandal anti-runway bombs, AM-500 sea mines , RADEOM Radar jamming pod[source] | — |
|---|
| Country of origin | Yugoslavia[source] Romania[source] | — |
|---|
| National origin | — | Russia[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Number built | — | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[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]