| 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 | |
