Su-35BM Specifications
| Specifications | ||
|---|---|---|
| Su-35BM | ||
| Length | 21.9 m | |
| Wing span | 15.3 m | |
| Height | 5.9 m | |
| T-O weight (max), kg | 34000 | |
| Take-off weight,- normal (2 x RVV-AE + 2 x R-73E) | 25,300 kg | |
| Maximal fuel load in internal fuel tanks, spec. weight 0.785 g/cu.cm (normal/max) | 11,500 kg | |
| Max landing weight, kg | ||
| Propulsion | 2 14,500 kg thrust By-pass turbojet engine | |
| Maximum speed | ||
| Speed of cruise | mach 1,05 (super-cruise) | |
| Radius of action at sea level, ?=0, ?=0.7 | 1580km | |
| Radius of action at maximum altitude, ?cr, ? cr | 3.600km | |
| Radius of action with 2 ? PTB-2000 external tanks | 4.500km | |
| Max flight range with internal fuel reserve, km | ||
| Max flight range with one in-flight refuelling, km | ||
| Max T-O run at normal T-O weight (full afterburner) | m 400-450 | |
| Max landing run on concrete runway in braking mode with brake parachute and wheel brakes use, with standard landing weight | m 650 | |
| Service ceiling, m | 18.800m | |
| Load factor limit, g | g 9 | |
| Rate of climb (?=1,000 m) | =280 m/sec | |
| Rate of turn: | * 32º/s | |
| Rate of rolling: | *270º/s | |
| Acceleration time at H=1,000 m and fuel bingo 50% of the standard capacity |
| |
| Weaponry Options | ||
| Capacity of weapons | 8,000 kg | |
| Hard points | 12 | |
| Armament |
| |
| Combat Potential |
Air-to-air mode
Air-to-surface mode | |
