| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
18.3
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
31.9
925
|
|
| Wingspan (Beam) (m) |
0.1
10.0
95
|
|
| Weights | ||
| Empty weight (kg) |
8
8,274
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
11,470
575,000
|
|
| Loaded weight (kg) |
5
10,950
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
2,050
28,165
|
at 11400 m |
| Fuel | ||
| Fuel Capacity (l) |
23
2,000
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
61.6
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
21,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,470
40,700
|
at 12000 m |
| Dynamic Performance | ||
| Load factor from (G) |
2
9
9
|
|
| Time to altitude (min) |
0.6
0.9
105
|
to 6000 m |
|
0.6
3.1
105
|
to 11000 m | |
| Combat | ||
| Missiles (qt) |
1
2
24
|
Kaliningrad K-8 |
| Stat | ||
| Introduction | 1958 | |
| First flight | 1958 | |
