Type | Aircraft | |
Company | Russian Aircraft Corporation MiG | |
Scheme | Integrated Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
17.4
88.7
|
|
Height (m) |
0.6
4.7
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
38.1
925
|
|
Wingspan (Beam) (m) |
0.1
11.4
95
|
|
Wing loading (kg/m2) |
3.1
403
829
|
|
Weights | ||
Empty weight (kg) |
8
11,000
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
20,000
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Hardpoints (qt) |
1
7
2,576
|
6 x pylons under-wing, 1 x under fuselage |
Speeds | ||
Ground Speed (km/h) |
96.6
1,500
1,500
|
|
Max. Speed (km/h) |
25
2,400
28,165
|
At high altitude |
Fuel | ||
Fuel External (l) |
142.5
3,800
10,025
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
1.1
2.1
|
|
Afterburning thrust (kN/kg) |
29.4
162.8
980
|
2 powerplants 81,4 kN each |
Performance | ||
Service ceiling (m) |
0.6
18,013
161,544
|
|
Range (Ferry range) (km) |
4
1,430
40,700
|
with 100% fuel |
Range PTB (Ferry range) (km) |
720
2,100
10,000
|
|
Dynamic Performance | ||
Load factor from (G) |
2
9
9
|
|
Rate of climb (m/min) |
1.9
19,800
36,000
|
initial |
Combat | ||
Guns (qt) |
1
1
18
|
30 mm GSh-30-1 cannon with 150 rounds |
Bombs weight (kg) |
2
3,500
39,000
|
|
Stat | ||
Number built (qt) |
0
1,600
43,000
|
|
Price (USD) |
41.5
29.0 million
750.0 million
|
|
Introduction | 2001 | |
First flight | 06.10.1977 |