| Company | Breguet Aviation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.5
88.7
|
|
| Height (m) |
0.6
4.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
19.5
925
|
|
| Wingspan (Beam) (m) |
0.1
7.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
3,793
276,800
|
|
| Loaded weight (kg) |
5
6,545
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,128
1,500
|
|
| Max. Speed (km/h) |
25
1,126
28,165
|
|
| Power | ||
| Afterburning thrust (kN/kg) |
29.4
29.4
980
|
2 powerplants 14,71 kN each |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| First flight | 31.03.1957 | |
