Type | Aircraft | |
Company | Russian Aircraft Corporation MiG | |
Scheme | Monoplane Midwing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
14.9
88.7
|
|
Wings | ||
Wing area (m2) |
1.1
23.1
925
|
|
Wingspan (Beam) (m) |
0.1
7.2
95
|
|
Weights | ||
Empty weight (kg) |
8
5,670
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
8,200
575,000
|
|
Loaded weight (kg) |
5
6,800
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
2,230
28,165
|
at 12000 m |
Fuel | ||
Fuel Capacity (l) |
23
3,200
320,000
|
|
Power | ||
Afterburning thrust (kN/kg) |
29.4
70.6
980
|
1 powerplant |
Thrust (kN) |
1.5
46.1
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
20,000
161,544
|
|
Combat | ||
Missiles (qt) |
1
2
24
|
Vympel K-13 air-to-air missiles (planned) |
Stat | ||
Number built (qt) |
0
2
43,000
|
|
Introduction | 1962 | |
First flight | 1962 |