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 |