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At a glance
Measured figures
Empty; Su-34 · Empty weight
Single sourceGross; Su-34 · Gross weight
Single sourceMaximum take-off; Su-34 · Max takeoff weight
Single source22,500 kg (49,604 lb)[source]
39,000 kg (85,980 lb)[source]
45,100 kg (99,428 lb)[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]
Cruise; Su-34 · Cruise speed
Single sourceMaximum; Su-34 · (Mach 1.8) at altitude
Single source1,900 km/h (1,200 mph, 1,000 kn) (Mach 1.8) at altitude[source]
1,300 km/h (810 mph, 700 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; Su-34 · Ferry range
Single source4,500 km (2,800 mi, 2,400 nmi)[source]
Su-34 · 2 × Saturn AL-31FM1 afterburning turbofan engines with afterburner
Single source2 × Saturn AL-31FM1 afterburning turbofan engines, 132 kN (30,000 lbf) with afterburner[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 · 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.
Configuration
| Specification | Sukhoi Su-34 | Sukhoi Su-57 |
|---|---|---|
| Type | Fighter-bomber / strike fighter[source] | Stealth multirole fighter[source] |
| National origin | Soviet Union / Russia[source] | Russia[source] |
| Manufacturer | Sukhoi , Novosibirsk Aircraft Production Association (NAPO)[source] | United Aircraft Corporation[source] |
| Status | In service[source] | In production[source] |
| Primary users | Russian Aerospace Forces Algerian Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
| Number built | >163 (7 test and 156 serial aircraft in early 2024)[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
| Manufactured | 2006–present[source] | 2019–present[source] |
| Introduction date | 20 March 2014[source] | 2020[source] |
| First flight | 13 April 1990 ( 1990-04-13 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
| Developed from | Sukhoi Su-27[source] | — |
| Fuel capacity | 12,100 kg (26,676 lb) internals[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 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 180 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[source] |
| Airfoil | 5%[source] | — |
| g limits | + 9[source] | +9.0[source] |
| Thrust/weight | 0.68[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
| Missiles | Air-to-air missiles : R-27 R/ER/T/ET R-73 R-77 Air-to-surface missiles : Kh-25 ML/MT Kh-29 L/T/D Kh-31 A/AD Kh-35 U Kh-38 MAE/MKE/MLE/MTE Kh-58 Kh-59 ME/MK/MK2 Kh-47M2 Anti-ship missiles : P-800 Oniks weight of 1500 kg with a range of up to 300 km and a speed in the range of numbers Mach 2.2–3.0. Officially not in service. Kh-41 Anti-radiation missiles : Kh-25 MP Kh-58 Kh-31 P/PD Cruise missiles : Kh-36 Grom-E1 Kh-65 S/SE Kh-SD[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 OFAB-250-270 bomb OFAB-100-120 bomb FAB-500T general-purpose bomb FAB-250 UMPK gliding bomb FAB-500 UMPK gliding bomb FAB-1500 UMPK gliding bomb FAB-3000 UMPK gliding bomb 2 × BETAB-500 SHP P-50T bomb ODAB-500PM bomb RBK-500 cluster bomb SPBE-D bomb UMPB D-30SN glide bomb[source] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
| Hardpoints | 12 × on wing and fuselage with a capacity of 12,000–14,000 kilograms (26,000–31,000 lb)[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] |
| Variant | — | Sukhoi/HAL FGFA (cancelled)[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] |