Company | Breguet Aviation | |
Scheme | Sesquiplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.3
88.7
|
|
Height (m) |
0.6
5.1
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
67.2
925
|
|
Wingspan (Beam) (m) |
0.1
20.2
95
|
|
Weights | ||
Empty weight (kg) |
8
3,500
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
7,200
575,000
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
310
28,165
|
|
Сruise Speed (km/h) |
52
285
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,300
60,000
|
2 powerplants 650 hp each |
Performance | ||
Service ceiling (m) |
0.6
10,000
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
14.6
36,000
|
|
Stat | ||
First flight | 1931 |