Type | Aircraft | |
Company | Russian Aircraft Corporation MiG | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
12.0
88.7
|
|
Height (m) |
0.6
4.4
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
17.7
925
|
|
Wingspan (Beam) (m) |
0.1
10.2
95
|
|
Aspect ratio |
1.7
5.7
25.6
|
|
Weights | ||
Max. takeoff weight (Gross weight) (kg) |
154
7,800
575,000
|
combat |
Loaded weight (kg) |
5
4,610
242,500
|
training |
Capacity | ||
Crew (per.) |
1
2
112
|
|
Hardpoints (qt) |
1
7
2,576
|
with a capacity of 2,000 kg |
Speeds | ||
Max. Speed (km/h) |
25
1,000
28,165
|
at 2500 m |
Fuel | ||
Fuel Capacity (l) |
23
2,390
320,000
|
|
Power | ||
Thrust (kN) |
1.5
34.5
1,914
|
2 powerplants 17,27 kN each |
Performance | ||
Service ceiling (m) |
0.6
14,000
161,544
|
|
Range (Ferry range) (km) |
4
1,200
40,700
|
|
Range PTB (Ferry range) (km) |
720
2,000
10,000
|
|
Dynamic Performance | ||
Load factor from (G) |
2
8
9
|
|
Rate of climb (m/min) |
1.9
4,902
36,000
|
|
Stat | ||
Number built (qt) |
0
2
43,000
|
|
Introduction | 1996 | |
First flight | 16.03.1996 |