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 |