| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Monoplane Midwing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
10.1
88.7
|
|
| Height (m) |
0.6
3.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
20.6
925
|
|
| Wingspan (Beam) (m) |
0.1
10.1
95
|
|
| Wing loading (kg/m2) |
3.1
240.8
829
|
|
| Weights | ||
| Empty weight (kg) |
8
3,630
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
6,105
575,000
|
|
| Loaded weight (kg) |
5
5,000
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,047
1,500
|
|
| Max. Speed (km/h) |
25
1,021
28,165
|
at 5000 m |
|
25
941
28,165
|
at 10000 m | |
| Сruise Speed (km/h) |
52
850
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,420
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.0
2.1
|
|
| Performance | ||
| Service ceiling (m) |
0.6
15,500
161,544
|
|
| Range (Ferry range) (km) |
4
1,335
40,700
|
|
| Takeoff roll (m) |
20
605
3,200
|
|
| Landing roll (m) |
20
755
2,570
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
966
36,000
|
at 10000 m |
|
1.9
2,460
36,000
|
at sea level | |
|
1.9
1,680
36,000
|
at 5000 m | |
| Time to altitude (min) |
0.6
6.8
105
|
to 10000 m |
|
0.6
2.4
105
|
to 5000 m | |
| Combat | ||
| Guns (qt) |
1
3
18
|
2x NR-23 23 mm (0.906 in) cannon in the lower left fuselage; 1x Nudelman N-37 37 mm (1.457 in) cannon in the lower right fuselage |
| Bombs (qt) |
1
2
250
|
100 kg (220 lb) bombs, drop tanks, or unguided rockets |
| Stat | ||
| Number built (qt) |
0
12,000
43,000
|
|
| Introduction | 1947 | |
| First flight | 30.12.1947 | |
