Credit
Alexander Mishin · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Su-24MK · Length
Single source22.53 m (73 ft 11 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Sukhoi Su-24 | Sukhoi Su-57 |
|---|---|---|
| Type | All-weather tactical bomber / interdictor[source] | Stealth multirole fighter[source] |
| National origin | Soviet Union / Russia[source] | Russia[source] |
| Manufacturer | Sukhoi[source] | United Aircraft Corporation[source] |
| Status | In service[source] | In production[source] |
20.1 m (65 ft 11 in)[source]
Empty; Su-24MK · Empty weight
Single sourceGross; Su-24MK · Gross weight
Single sourceMaximum take-off; Su-24MK · Max takeoff weight
Single source22,300 kg (49,163 lb)[source]
38,040 kg (83,864 lb)[source]
43,755 kg (96,463 lb)[source]
Empty; Su-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; Su-24MK · / M1.6 at high altitude
Single source1,654 km/h (1,028 mph, 893 kn) / M1.6 at high altitude[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; Su-24MK · Ferry range
Single source2,775 km (1,724 mi, 1,498 nmi)[source]
Su-24MK · 2 × Lyulka AL-21F-3A turbojet engines thrust each dry
Single sourceSu-24MK · with afterburner
Single source2 × Lyulka AL-21F-3A turbojet engines, 75 kN (17,000 lbf) thrust each dry, 109.8 kN (24,700 lbf) with afterburner[source]
Su-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceSu-24MK · 30,000 ft/min
Single source150 m/s (30,000 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 | Russian Aerospace Forces Ukrainian Air Force Islamic Republic of Iran Air Force Algerian Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | Approximately 1,400[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 1967–1993[source] | 2019–present[source] |
|---|
| Introduction date | 1974[source] | 2020[source] |
|---|
| First flight | T-6: 2 July 1967 ( 1967-07-02 ) T-6-2I: 17 January 1970 ( 1970-01-17 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | Sukhoi S-6[source] | — |
|---|
| Fuel capacity | 11,100 kg (24,471 lb)[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 × internal 23 mm Gryazev-Shipunov GSh-6-23 M rotary cannon with 500 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
|---|
| Hardpoints | 9 hardpoints with a capacity of up to 8,000 kg (17,635 lb), with provisions to carry combinations of: Rockets: S-5 S-8 S-13 S-24 B S-25 -OFM/LD Missiles: Air-to-air missiles : 4 × R-60 MK 4 × R-73 E Air-to-surface missiles : 4 × Kh-23 M 4 × Kh-25 ML Kh-59 ME Kh-29 L/T/D Anti-ship missiles : Kh-31 A Anti-radiation missiles : 2 × Kh-28 2 × Kh-58 E Kh-25 MP 2 × Kh-31 P Kh-27 PS Bombs: KAB-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500OD guided bomb KAB-500S-E satellite-guided bomb KAB-1500KR TV-guided bomb KAB-1500L laser-guided bomb ODAB-500 PM bomb RBK-250 cluster bomb RBK-500 cluster bomb 2 × BETAB-500 bomb[source] | 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| Airfoil | TsAGI SR14S-5.376; TsAGI SR16M-10[source] | — |
|---|
| g limits | + 6[source] | +9.0[source] |
|---|
| Wing loading | 651 kg/m 2 (133 lb/sq ft)[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | 0.6[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Rockets | S-5 S-8 S-13 S-24 B S-25 -OFM/LD[source] | — |
|---|
| Missiles | Air-to-air missiles : 4 × R-60 MK 4 × R-73 E Air-to-surface missiles : 4 × Kh-23 M 4 × Kh-25 ML Kh-59 ME Kh-29 L/T/D Anti-ship missiles : Kh-31 A Anti-radiation missiles : 2 × Kh-28 2 × Kh-58 E Kh-25 MP 2 × Kh-31 P Kh-27 PS[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 | KAB-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500OD guided bomb KAB-500S-E satellite-guided bomb KAB-1500KR TV-guided bomb KAB-1500L laser-guided bomb ODAB-500 PM bomb RBK-250 cluster bomb RBK-500 cluster bomb 2 × BETAB-500 bomb[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[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]
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]