Type | Aircraft | |
Company | Breguet Aviation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
15.9
88.7
|
|
Height (m) |
0.6
5.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
56.3
925
|
|
Wingspan (Beam) (m) |
0.1
20.5
95
|
|
Weights | ||
Empty weight (kg) |
8
4,840
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
8,600
575,000
|
|
Loaded weight (kg) |
5
8,200
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Capacity passengers (per.) |
1
12
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
385
28,165
|
at 1600 m |
Сruise Speed (km/h) |
52
340
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,608
60,000
|
2 powerplants 804 hp each |
Performance | ||
Service ceiling (m) |
0.6
6,000
161,544
|
|
Range (Ferry range) (km) |
4
1,000
40,700
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
7
105
|
to 1500 m |
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1936 | |
First flight | 05.03.1936 |