| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
22.7
88.7
|
|
| Height (m) |
0.6
6.2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
61.6
925
|
|
| Wingspan (Beam) (m) |
0.1
13.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
21,820
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
46,200
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
pilot and weapons system officer |
| Hardpoints (qt) |
1
8
2,576
|
6 for rockets and 2 for external fuel tanks |
| Speeds | ||
| Max. Speed (km/h) |
25
3,000
28,165
|
High altitude |
| Сruise Speed (km/h) |
52
2,500
3,087
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.9
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
304
980
|
2 powerplants 152 kN each |
| Thrust (kN) |
1.5
186
1,914
|
2 powerplants 93 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
20,600
161,544
|
|
| Range (Ferry range) (km) |
4
3,000
40,700
|
|
| Сombat radius (km) |
277
1,450
7,210
|
|
| Dynamic Performance | ||
| Load factor from (G) |
2
5
9
|
|
| Rate of climb (m/min) |
1.9
12,480
36,000
|
|
| Combat | ||
| Guns (qt) |
1
1
18
|
GSh-6-23 23 mm cannon with 260 rounds. |
| Stat | ||
| Number built (qt) |
0
519
43,000
|
|
| Introduction | 1985 | |
| First flight | 16.09.1975 | |
