| length | 17.75-22.0 m,
|
| height | 5.08 m,
|
| wingspan | 16.9 m,
|
| wing area | 63.5 m2.
|
| mass of the empty plane | 13,000 kg.
|
| - normal take-off | 18,000 kg
|
| Maximum take-off weight | 22,000 kg.
|
| mass of fuel in internal tanks | 3700-4000 kg.
|
| mass of fuel in PTB, l | 2 x 800 l - 1930
|
| power plant | 2 DTRD RD-33I,
|
| Thrust traction | 2 x 5320 kgf.
|
| Maximum speed | 1100 km / h
|
| Cruising speed | 950 km / h
|
| Practical flight range | 1000 km.
|
| Practical range at high speed | 750-800 km
|
| Combat radius of action | 250-300 / 400-500 km
|
| Ferry range | 3000 km.
|
| Practical ceiling | 9,600-10,000 m.
|
| Armament |
1 twin 30 mm 9A-4071K cannon rotatable in the vertical plane (500 rounds, 1,500 rounds / min),
2 x 23 mm GSh-2-23 in a movable installation in the tail (60 rounds, 2,400-3200 rounds / min).
|
| Maximum combat load | 7200 kg at 16 points of suspension (including 6 compartments in the wing for
bombs of caliber 250 kg).
free-falling and guided bombs, up to 500 kg.
UR "air-to-air" - R-60M and R-73,
UR "air-to-surface" - X-23, X-25, X-29, X-58.
All types of NARs,
cannon containers UAK-23-250, SPPU-1-23.
|
| Crew | 2 people (pilot, gunner-operator).
|
