Sukhoï Su-57
| GENERAL DATA | |||
| Type |
Stealth air superiority fighter
|
Other Designation | Sukhoï T-50-I PAK FA |
| Manufacturer(s) | Sukhoi |
||
| Prototype first flight | 29 January 2010 |
Introduction | 2019 (planned) |
| Produced | 2009–present |
Number built | 10 flyable prototypes |
| Status | In serial production |
Crew | 1-2 |
| DIMENSIONS | |||
| Length | 20.1 m |
Empty Weight | 18000 kg |
| Wingspan | 14.1 m |
Loaded Weight | 25000 kg typical mission weight, 29270 kg at full load |
| Height | 4.74 m |
Max takeoff weight | 35000 kg |
| Wing area | 78.8 m² |
Wing loading | 317 kg/m² typical mission weight, 470 kg/m² maximum |
| ARMAMENT | |||
| Guns | 1 × 30 mm Gryazev-Shipunov
GSh-30-1 autocannon in right LEVCON root |
Ammunition Carried |
? |
| Hardpoints | 12 hardpoints (6 × internal,
6 × external)
|
||
| Air-to-surface missiles | 4 × Kh-38ME, Kh-59MK2 |
||
| Anti-ship missiles | 2 × Kh-35E, 31 etc |
||
| Air-to-air missiles | 4 × RVV-MD, 2 × R-73,
R-37M |
||
| Anti-radiation missiles | 4 × Kh-58UShKE, 250- 500-1500
kg guided bombs, Anti-tank "Drill" 500 kg cluster-bomb
+ active homing |
||
| POWERPLANT (initial production) | |||
| Engine | 2 ×
Saturn AL-41F1 turbofans with thrust vectoring
|
||
| Dry thrust | 93.1 kN each |
Thrust with afterburner | 147.2 kN each |
| Thrust/weight | 1.19 at typical mission
weight
|
Fuel Capacity | 10300 kg internally |
| POWERPLANT (later production) | |||
| Engine | 2 ×
izdeliye 30 turbofans with thrust vectoring
|
||
| Dry thrust | 107.9 kN each |
Thrust with afterburner | 176.6 kN each |
| Thrust/weight | 1.15–1.2(1.36 at
typical mission weight)
|
Fuel Capacity | 10300 kg internally |
| PERFORMANCES | |||
| Maximum Speed | Mach 2
(2120 km/h) at altitude |
Supercruise | Mach 1.6 (1710 km/h)
at altitude |
| Stall Speed | 250 km/h |
Climbing speed | 350 m/s |
| Subsonic range | 3500 km, 4500 km from 2 outboard
fuel tanks
|
||
| Supersonic Range | 1500 km |
Service ceiling | 20000 m |
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
