| Year of release | 1954 | 1955 |
| engine type |
AL-7 |
AL-7F |
| rising thrust, kgs |
2 @ 8600 |
2 @ 10,000 |
| total takeoff thrust, kgs |
17 200 |
20,000 |
| Dimensions | | |
| Wingspan, m | 17.65
|
| Length m | 28.96
|
| Height, m | 7.90
|
| Wing area, m2 | 84.60
|
| Weights | | |
| empty, kg | 24000 | |
| flight normal, kg | 36 820 | 40 660 |
| flight maximum, kg | 38,000 | 41 600 |
| Flight characteristics | | |
| Speed km / h |
|
| cruising | 910
|
| maximum at height | 1250
|
| maximum near the ground | 1155
|
| maximum speed, km/h | 1050 | 1155 |
| at altitude of 5,000 meters (16,000 ft), km/h |
1,150 km/h (710 mph, 620 kn)
| 1,250 km/h (780 mph; 670 kn)
|
| time to 5,000 meters, minutes | | 1,1 |
| practical ceiling, m | 13,000 (43,000 ft) | 14,000 (46,000 ft) |
| flight range, km | 2500 | 3000 |
| at speed, km/h | 910 | 910 |
| with bomb load, kg | 3000 | 3000 |
| Runway characteristics | | |
| run on takeoff, m | 1075 | 1075 |
| landing speed, km/h | 243 | 243 |
| landing distance, m | 1150 | 1150 |
| Weapon | | |
| bomb | | |
| normal, kg | 3000 | 3000 |
| maximum, kg | 5000 | 5000 |
| Armament: | 3 x 23 mm NR-23 or two 23-mm guns TKB-4957: to protect the front hemisphere, one fixed front gun mounted on the left side of the fuselage; in the rear of the fuselage of the aircraft a stern cannon mount (Il-K8) with a remote electro-hydraulic drive of two movable guns.
Bomb load on the internal suspension: normal - 3000 kg, maximum - 5000 kg.
|
| Crew | 3
|
