Credit
Anna Zvereva from Tallinn, Estonia · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Su-57E · Length
Single source20.1 m (65 ft 11 in)[source]
Configuration
| Specification | Sukhoi Su-57 | Tupolev PAK DA |
|---|---|---|
| Type | Stealth multirole fighter[source] | Stealth strategic bomber[source] |
| National origin | Russia[source] | Russia[source] |
| Manufacturer | United Aircraft Corporation[source] | Kazan Aircraft Production Association , Novosibirsk Aircraft Production Association Plant , Beriev[source] |
| Designer | Sukhoi[source] | Tupolev |
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.
| Built by | Komsomolsk-on-Amur Aircraft Plant[source] | — |
|---|
| Status | In production[source] | In development[source] |
|---|
| Primary users | Russian Aerospace Forces Algerian Air Force[source] | — |
|---|
| Number built | 44+ as of 2026 (including 10 test aircraft)[source] | — |
|---|
| Manufactured | 2019–present[source] | — |
|---|
| Introduction date | 2020[source] | 2027 (expected)[source] |
|---|
| First flight | 29 January 2010 ( 2010-01-29 )[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] | — |
|---|
| Primary user | — | Russian Aerospace Forces[source] |
|---|
| Source measurement | — | The Tupolev PAK DA or PAK DA ( Russian : ПАК ДА , short for: Перспективный авиационный комплекс дальней авиации , romanized : Perspektivnyi aviatsionnyi kompleks dal'ney aviatsii , lit. ' 'Prospective aviation complex for long-range aviation ' ' ), codename Poslannik ( Russian : Посланник , lit. ' Envoy ' ), is a next-generation stealth strategic bomber being developed by Tupolev for the Long-Range Aviation branch of the Russian Aerospace Forces . The PAK DA is set to complement and eventually replace the older Tupolev Tu-95 in Russia's Air Force service.[source]Tupolev PAK DA · Lead; only the objects and conditions stated in this passage Technical parameters of the PAK DA include subsonic speed, 12,000-kilometre (7,500 mi) operational range and a capability to continuously remain in the air for up to 30 hours while carrying both conventional and nuclear payloads up to 30 tons. The aircraft is expected to have a crew of four.[source]Tupolev PAK DA · Lead; only the objects and conditions stated in this passage In July 2018, United Engine Corporation (UEC) and Tupolev signed a contract for the creation of PAK DA's powerplant. According to early reports, it will be derived from the upgraded Kuznetsov NK-32 Tier 2 engine, intended for modernized Tu-160M2s. About RUB8 billion was to be allocated for the development of the new engine that will be produced by JSC Kuznetsov in Samara . The engine is to provide the PAK DA with a capability to perform 30 hours nonstop flight while being resistant to temperatures from minus 60°C to plus 50°C and even effects of a nuclear explosion. Its service life is expected to be from 12 to 21 years. The first tests of the PAK DA engine will take place in 2020 and be completed by the end of 2021.[source]Tupolev PAK DA · Development; only the objects and conditions stated in this passage |
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| Country of origin | — | Russia[source]Inventory Origin column; table 6, row 21, cell 2; revision 1364906102; retrieved 2026-10-02 |
|---|