| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.0
88.7
|
|
| Height (m) |
0.6
4.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
17.7
925
|
|
| Wingspan (Beam) (m) |
0.1
10.2
95
|
|
| Aspect ratio |
1.7
5.7
25.6
|
|
| Weights | ||
| Max. takeoff weight (Gross weight) (kg) |
154
7,800
575,000
|
combat |
| Loaded weight (kg) |
5
4,610
242,500
|
training |
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Hardpoints (qt) |
1
7
2,576
|
with a capacity of 2,000 kg |
| Speeds | ||
| Max. Speed (km/h) |
25
1,000
28,165
|
at 2500 m |
| Fuel | ||
| Fuel Capacity (l) |
23
2,390
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
34.5
1,914
|
2 powerplants 17,27 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
14,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,200
40,700
|
|
| Range PTB (Ferry range) (km) |
720
2,000
10,000
|
|
| Dynamic Performance | ||
| Load factor from (G) |
2
8
9
|
|
| Rate of climb (m/min) |
1.9
4,902
36,000
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1996 | |
| First flight | 16.03.1996 | |
