| Type | Aircraft | |
| Company | Breguet Aviation British Aircraft Corporation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.8
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
24
925
|
|
| Wingspan (Beam) (m) |
0.1
8.7
95
|
|
| Aspect ratio |
1.7
3.1
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
7,000
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
15,700
575,000
|
|
| Loaded weight (kg) |
5
10,954
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
5
2,576
|
4×under-wing and 1× center-line pylon stations |
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,300
1,500
|
|
| Max. Speed (km/h) |
25
1,699
28,165
|
at 11000 m |
| Power | ||
| Afterburning thrust (kN/kg) |
29.4
65
980
|
2 powerplants 32,5 kN |
| Thrust (kN) |
1.5
45.5
1,914
|
2 powerplants 22,75 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
14,000
161,544
|
|
| Range (Ferry range) (km) |
4
4,210
40,700
|
|
| Сombat radius (km) |
277
908
7,210
|
lo-lo-lo, external fuel |
| Dynamic Performance | ||
| Load factor from (G) |
2
7.5
9
|
|
| Time to altitude (min) |
0.6
1.5
105
|
to 9145 m |
| Combat | ||
| Guns (qt) |
1
2
18
|
30 mm (1.18 in) DEFA cannons |
| Rockets (qt) |
1
8
76
|
Matra rocket pods |
| Stat | ||
| Number built (qt) |
0
543
43,000
|
|
| Price (USD) |
41.5
8.0 million
750.0 million
|
|
| Introduction | 1969 | |
| First flight | 08.09.1968 | |
| Stop production | 2005 | |
