Sukhoï Su-47 Berkut
| GENERAL DATA | |||
| Type |
Experimental aircraft/
Technology demonstrator |
Other Designation | S-32, S-37, Firkin (NATO) |
| Manufacturer(s) | Sukhoi |
||
| Prototype first flight | 25 September 1997 |
Status | Cancelled |
| Number built | 4 flight testing prototypes |
Crew | 1 |
| DIMENSIONS | |||
| Length | 22.6 m |
Empty Weight | 16 375 kg |
| Wingspan | 6.7 m |
Loaded Weight | 25670 kg |
| Height | 6.4 m |
Max takeoff weight | 34000 kg |
| Wing area | 61.87 m² |
Wing loading | 458 kg/m² typical mission weight, 607 kg/m² maximum |
| ARMAMENT | |||
| Guns | 1 × 30 mm Gryazev-Shipunov
GSh-30-1 autocannon in right LEVCON root |
Ammunition Carried |
150 |
| Inside | 3 R-33 missiles mounted on a launcher
in an internal cargo bay
|
||
| Outside | Up to 8000 kg externally spread
over 14 hardpoints |
||
| POWERPLANT | |||
| Engine | 2 ×
Aviadvigatel PS-30F6 afterburning turbofan engines
|
||
| Dry thrust | 93.1 kN each |
Thrust with afterburner | 147.2 kN each |
| Thrust/weight | 1.77 at typical mission
weight,
1.16 max take-off weight |
Fuel Capacity | ? kg internally |
| PERFORMANCES | |||
| Maximum Speed | Mach 2.21
(2200 km/h) at altitude |
Supercruise | Mach 1.12 (1400 km/h)
at sea level |
| Rate of climb | 233 m/s |
Service ceiling | 18000 m |
| Range | 3300 km
|
||
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
