Company | Breguet Aviation | |
Scheme | Monoplane Midwing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
9
88.7
|
|
Wings | ||
Wing area (m2) |
1.1
20
925
|
|
Wingspan (Beam) (m) |
0.1
20.0
95
|
|
Wing loading (kg/m2) |
3.1
34.5
829
|
|
Aspect ratio |
1.7
20
25.6
|
|
Weights | ||
Empty weight (kg) |
8
340
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
690
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Stall Speed (km/h) |
40
62
257.7
|
|
Never exceed speed (km/h) |
108.0
220
1,050
|
|
Performance | ||
Maximum glide ratio |
7
35
43
|
|
Dynamic Performance | ||
Rate of sink (m/min) |
36
42
55.8
|
|
Stat | ||
Number built (qt) |
0
18
43,000
|
|
First flight | 26.05.1956 |