| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
9.8
88.7
|
|
| Height (m) |
0.6
3.2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
18.2
925
|
|
| Wingspan (Beam) (m) |
0.1
10
95
|
|
| Wing loading (kg/m2) |
3.1
278
829
|
|
| Weights | ||
| Empty weight (kg) |
8
3,350
276,800
|
|
| Loaded weight (kg) |
5
5,000
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
864
1,500
|
|
| Max. Speed (km/h) |
25
915
28,165
|
|
| Never exceed speed (km/h) |
108.0
1,050
1,050
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,625
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
15.6
1,914
|
2 powerplants 7,8 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
13,500
161,544
|
|
| Range (Ferry range) (km) |
4
800
40,700
|
at 10000 m |
| Takeoff roll (m) |
20
950
3,200
|
with total weight of 4950 kg |
| Landing roll (m) |
20
1,060
2,570
|
with total weight of 3760 kg |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
1,320
36,000
|
|
| Time to altitude (min) |
0.6
4.3
105
|
to 5000 m |
|
0.6
10.8
105
|
to 10000 m | |
| Combat | ||
| Guns (qt) |
1
3
18
|
1 × 37 mm Nudelman N-37 cannon; 2 × 23 mm Nudelman-Suranov NS-23 cannon |
| Stat | ||
| Number built (qt) |
0
610
43,000
|
|
| Introduction | 1949 | |
| First flight | 24.04.1946 | |
