Type | Aircraft | |
Company | Breguet Aviation | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
24.4
88.7
|
|
Height (m) |
0.6
8.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
173.1
925
|
|
Wingspan (Beam) (m) |
0.1
40.4
95
|
|
Wing loading (kg/m2) |
3.1
165
829
|
|
Weights | ||
Empty weight (kg) |
8
16,134
276,800
|
|
Loaded weight (kg) |
5
28,660
242,500
|
|
Capacity | ||
Crew (per.) |
1
10
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
330
28,165
|
|
Сruise Speed (km/h) |
52
230
3,087
|
|
Power | ||
Total Power (hp) |
0.4
4,480
60,000
|
4 powerplants 1120 hp each |
Performance | ||
Service ceiling (m) |
0.6
6,000
161,544
|
|
Range (Ferry range) (km) |
4
6,923
40,700
|
|
Endurance (h) |
0.0
0.5
150
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
9
105
|
to 3000 m |
Stat | ||
Number built (qt) |
0
5
43,000
|
|
Introduction | 1938 | |
First flight | 04.04.1938 | |
Stop production | 1954 |