| 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 | |
