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 |