Type | Aircraft | |
Company | Canadair Lockheed Corporation | |
Geometry | ||
---|---|---|
Length (m) |
1.9
16.7
88.7
|
|
Height (m) |
0.6
4.1
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
6.6
95
|
|
Weights | ||
Empty weight (kg) |
8
6,350.3
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
13,171.4
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
1,844
28,165
|
|
Power | ||
Afterburning thrust (kN/kg) |
29.4
66.7
980
|
1 powerplant |
Thrust (kN) |
1.5
44
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
15,240
161,544
|
|
Range (Ferry range) (km) |
4
2,630
40,700
|
|
Combat | ||
Guns (qt) |
1
1
18
|
20 mm (0.79 in) M61A1 Vulcan cannon |
Stat | ||
Number built (qt) |
0
200
43,000
|
|
First flight | 26.05.1961 | |
Stop production | 1995 |