Wing span,m
Lenght, m
Fuselage lenght, m
Height, m
Wing area, m22
Weight, ,kg
- Empty
fuel
- Normal take-off,kg
- Maximum take-off
Engines
Thrust, kN:
dry
afterburner
Max. speed, km/h
- in altitude
- on sea level
Rate of climb, m/s
Service ceiling, m
Range, m
- without AFT
- with AFT
Max. overload
Hardpoints
Cannons, mm |
7,154
13,460
12,177
4806
23,000
-
1790
6850
-
R-11
F300
38,0
56,3
2175
1100
130
19000
1520
-
7,0
3
2,30 |
7,154
13,460
12,177
4,806
23,000
4980
2115
7370
8625
R-11
F300
38,2
56,3
2175
1150
130
19000
1300
1670
7,0
3
1,30 |
7,154
14,700
12,285
4,806
23,000
-
2280
7750
-
R-11
F2-300
38,7
60,0
2175
1300
-
19000
1400
1770
8,0
3
- |
7,154
14,700
12,285
4,806
23,000
-
2400
7830
9080
R-11
F300
38,0
56,3
2175
1300
-
18500
1450
1800
8,0
3
- |
7,154
14,700
12,285
4,710
23,000
-
2200
7820
-
R-11
F2-S300
38,2
60,5
2230
1300
-
19000
1300
1650
8,5
3
1,23 |
7,154
14,700
12,285
4,710
23,000
-
2320
8150
-
R-11
F2-S300
38,2
60,5
2230
1300
-
18000
1240
1610
8,5
5
1,23 |
7,154
14,700
12,285
4,710
23,000
-
2200
8300
9400
R -13-300
39,9
63,6
2230
1300
205
18000
1050
1420
8,5
5
1,23 |
7,154
14,700
12,285
4,710
23,000
5350
2200
8200
-
R-13-300
39,9
63,6
2230
1300
205
18200
1050
1420
8,5
5
1,23 |
7,154
14,700
12,285
4,710
23,000
-
2390
8725
10400
R-25-300
40,2
69,9
2175
1450
225
17800
1210
1470
8,5
5
1,23 |
7.154
14,700
12,285
4,710
23000
-
2390
8825
-
R-25-300
40,2
69,9
2175
1300
225
17500
1210
1470
8,5
5
2,23 |