| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.3
88.7
|
|
| Height (m) |
0.6
3.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
22.6
925
|
|
| Wingspan (Beam) (m) |
0.1
9.6
95
|
|
| Wing loading (kg/m2) |
3.1
237
829
|
|
| Weights | ||
| Empty weight (kg) |
8
3,919
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
6,069
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,070
28,165
|
at 5000 m |
|
25
1,145
28,165
|
at 3000 m | |
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
33.8
980
|
1 powerplant |
| Thrust (kN) |
1.5
26.5
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
16,600
161,544
|
|
| Range (Ferry range) (km) |
4
2,060
40,700
|
with drop tanks |
| Takeoff roll (m) |
20
550
3,200
|
|
| Landing roll (m) |
20
850
2,570
|
|
| Dynamic Performance | ||
| Load factor from (G) |
2
8
9
|
|
| Rate of climb (m/min) |
1.9
3,900
36,000
|
|
| Time to altitude (min) |
0.6
3
105
|
to 5000 m |
|
0.6
6.7
105
|
to 10000 m | |
|
0.6
14.3
105
|
to 15000 m | |
| Combat | ||
| Guns (qt) |
1
3
18
|
1x 37 mm Nudelman N-37 cannon; 2x 23 mm Nudelman-Rikhter NR-23 cannons |
| Stat | ||
| Number built (qt) |
0
11,060
43,000
|
|
| Introduction | 1953 | |
| First flight | 14.01.1950 | |
