| Type | Aircraft | |
| Company | Russian Aircraft Corporation MiG | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
17.1
88.7
|
|
| Height (m) |
0.6
5
50.1
|
|
| Wings | ||
| Wing loading (kg/m2) |
3.1
605
829
|
|
| Weights | ||
| Empty weight (kg) |
8
11,908
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
20,670
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
1
2,576
|
|
|
1
7
2,576
|
||
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,350
1,500
|
|
| Max. Speed (km/h) |
25
1,885
28,165
|
at 8000 m |
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
112.8
980
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
14,000
161,544
|
|
| Range (Ferry range) (km) |
4
2,500
40,700
|
Ferry range |
| Сombat radius (km) |
277
780
7,210
|
with two Kh-29 ASMs and three drop tanks lo-lo-lo |
|
277
540
7,210
|
with two Kh-29 ASMs and no external fuel lo-lo-lo | |
| Dynamic Performance | ||
| Load factor from (G) |
2
7
9
|
|
| Rate of climb (m/min) |
1.9
12,000
36,000
|
|
| Stat | ||
| Number built (qt) |
0
1,075
43,000
|
|
| Introduction | 1976 | |
| First flight | 20.08.1970 | |
