تويت
| Su-35 basic specifications | |
| Take-off weight, kg: | |
normal (2 x RVV-AE + 2 x R-73E) |
25,300 |
maximal |
34,500 |
| By-pass turbojet engine: | |
number, pcs |
2 |
thrust, kg |
14,500 |
| Maximal fuel load in internal fuel tanks, kg | 11,500 |
| Maximal combat load, kg | 8,000 |
| Ceiling, km | 18 |
| Range with maximal fuel load, km: | |
Н=0, М=0.7 |
1,580 |
Нcr, М cr |
3,600 |
| Ferry range: | 4,500 |
with 2 х PTB-2000 external tanks, km |
|
| Acceleration time at H=1,000 m and fuel bingo 50% of the standard capacity, sec: | |
from 600 km/h to 1,100 km/h |
13.8 |
from 1,100 km/h to 1,300 km/h |
8.0 |
| Maximal rate of climb (Н=1,000 m), m/sec | >280 |
| Maximal airspeed : | |
H=200 m, km/h |
1,400 |
H=11,000 m , M |
2.25 |
| Maximal g-load, g | 9 |
| Take-off run in "full afterburning" mode with standard take-off weight, m | 400-450 |
| Landing roll on concrete runway in braking mode with brake parachute and wheel brakes use, with standard landing weight, m | 650 |
| Length, m | 21.9 |
| Height, m | 5.9 |
| Wing span, m | 15.3 |
تعليق