Credit
U.S. Navy photo · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
F-14D · Length
Single source62 ft 9 in (19.13 m)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Grumman F-14 Tomcat | Sukhoi Su-57 |
|---|---|---|
| Type | Interceptor , air superiority , and multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | United States[source] | Russia[source] |
| Manufacturer | Grumman[source] | United Aircraft Corporation[source] |
| Status | In service with Iran[source] | In production |
20.1 m (65 ft 11 in)[source]
Empty; F-14D · Empty weight
Single sourceGross; F-14D · Gross weight
Single sourceMaximum take-off; F-14D · Max takeoff weight
Single source43,735 lb (19,838 kg)[source]
61,000 lb (27,669 kg)[source]
74,350 lb (33,725 kg)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceCruise; F-14D · Cruise speed
Single sourceMaximum; F-14D · at sea level
Single sourceMaximum; F-14D · Mach 2.34 at 40,000 ft (12,190 m) Mach 1.2
Single sourceMach 2.34, 1,544 mph (1,342 kn; 2,485 km/h) at 40,000 ft (12,190 m) Mach 1.2, 794 kn (914 mph; 1,470 km/h) at sea level[source]
420 kn (480 mph, 780 km/h)[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceF-14D · Range
Single source1,600 nmi (1,800 mi, 3,000 km)[source]
F-14D · deck launched intercept
Single sourceF-14D · fighter escort
Single sourceF-14D · fleet air defense with 1.91 hours of loiter
Single source503 nmi (579 mi, 932 km) fighter escort 204 nmi (235 mi; 378 km) deck launched intercept 150 nmi (170 mi; 280 km) fleet air defense with 1.91 hours of loiter[source]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[source]
F-14D · 2 × General Electric F110 -GE-400 afterburning turbofans thrust each dry
Single sourceF-14D · with afterburner
Single source2 × General Electric F110 -GE-400 afterburning turbofans , 16,333 lbf (72.65 kN) thrust each dry, 26,950 lbf (119.9 kN) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceF-14D · 45,000 ft/min ( ) plus
Single source45,000 ft/min (230 m/s) plus[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 | United States Navy (historical) Imperial Iranian Air Force (historical) Islamic Republic of Iran Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | 712[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 1969–1991[source] | 2019–present[source] |
|---|
| Introduction date | 22 September 1974 ( 1974-09-22 )[source] | 2020[source] |
|---|
| First flight | 21 December 1970 ( 1970-12-21 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Retired | 22 September 2006 ( 2006-09-22 ) ( United States Navy )[source] | — |
|---|
| Fuel capacity | 16,200 lb (7,348 kg) internal fuel; 2 × optional 267 US gal (222 imp gal; 1,010 L) / 1,756 lb (797 kg) external drop tanks[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] |
|---|
| Guns | 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled rotary cannon, with 675 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 10 total: 6× under-fuselage, 2× under nacelles and 2× on wing gloves with a capacity of 14,500 lb (6,600 kg) of ordnance and fuel tanks , with provisions to carry combinations of: Rockets: 7x LAU-10 rocket pods (for a total of 28 rockets) Missiles: AIM-54 Phoenix , AIM-7 Sparrow , AIM-9 Sidewinder air-to-air missiles Bombs: JDAM precision-guided munition (PGMs) Paveway series of laser-guided bombs Mk 80 series of unguided iron bombs Mk 20 Rockeye II cluster munition Other: Tactical Airborne Reconnaissance Pod System (TARPS) LANTIRN Targeting System (LTS) pod (AN/AAQ-14) 2× 267 US gal (1,010 L; 222 imp gal) drop tanks for extended range/loitering time[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Swept wingspan | 38 ft 2.5 in (11.646 m) swept[source] | — |
|---|
| Airfoil | Grumman (1.74)(35)(9.6)-(1.1)(30)(1.1) root Grumman (1.27)(30)(9.0)-(1.1)(40)(1.1) tip[source] | — |
|---|
| Stall speed | 118 kn (136 mph, 219 km/h) power-off[source] | — |
|---|
| g limits | +7.5 g (+6.5 g operational limit)[source] | +9.0[source] |
|---|
| Wing loading | 96 lb/sq ft (470 kg/m 2 ) 48 lb/sq ft (230 kg/m 2 ) effective[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | 0.88 at gross weight (1.02 with loaded weight & 50% internal fuel)[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Takeoff roll | 2,500 ft (760 m)[source] | — |
|---|
| Landing roll | 2,400 ft (730 m)[source] | — |
|---|
| Rockets | 7x LAU-10 rocket pods (for a total of 28 rockets)[source] | — |
|---|
| Missiles | AIM-54 Phoenix , AIM-7 Sparrow , AIM-9 Sidewinder air-to-air 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] |
|---|
| Bombs | JDAM precision-guided munition (PGMs) Paveway series of laser-guided bombs Mk 80 series of unguided iron bombs Mk 20 Rockeye II cluster munition[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Other | Tactical Airborne Reconnaissance Pod System (TARPS) LANTIRN Targeting System (LTS) pod (AN/AAQ-14) 2× 267 US gal (1,010 L; 222 imp gal) drop tanks for extended range/loitering time[source] | — |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | Komsomolsk-on-Amur Aircraft Plant[source] |
|---|
| Variant | — | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[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]
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]