     
|
| Weight |
| kg | lb |
| Maximum take-off weight |
21500 |
52438 |
| Normal take-off weight |
16950 |
41341 |
|
|
|
| Delivery ordnance |
| |
kg |
lb |
| Maximum |
4000 |
9756 |
| |
|
|
| Flight speed |
|
km/h |
knots |
| Maximum |
950 |
513 |
| Minimum |
175 |
94,5 |
|
|
|
| Rate-of-climb |
| |
m/s |
ft/min |
| Maximum |
65 |
12795 |
|
|
|
| Flight range |
| |
km |
nm |
| Maximum radius of combat employment («high altitude – high altitude») |
1050 |
567 |
| Ferry |
2200 |
1189 |
|
|
|
| Flight ceiling |
|
m |
ft |
| Service ceiling |
12000 |
39370 |
|
|
|
| Takeoff run |
|
m |
ft |
| On concrete runway |
600 |
1970 |
| On unpaved runway |
700 |
2300 |
|
|
|
| Landing run |
|
m |
ft |
| On concrete runway |
550 |
1805 |
| On unpaved runway |
600 |
1970 |
|
|
|
| Engine thrust |
|
êãñ |
kgf |
| Resultant thrust 2 õ R-195 |
2 õ 4500 |
2 x 4500 |
|