Company | Société des avions Caudron | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
6.6
88.7
|
|
Wings | ||
Wing area (m2) |
1.1
7
925
|
|
Wingspan (Beam) (m) |
0.1
6.8
95
|
|
Wing loading (kg/m2) |
3.1
100
829
|
|
Rotors | ||
Rotor number (qt) |
1
2
8
|
|
Weights | ||
Empty weight (kg) |
8
405
276,800
|
|
Loaded weight (kg) |
5
695
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
350
28,165
|
|
Fuel | ||
Fuel Capacity (l) |
23
280
320,000
|
|
23
280
320,000
|
||
Propellers | ||
Prop blade number (qt) |
1
2
8
|
|
Stat | ||
Number built (qt) |
0
3
43,000
|
|
First flight | 1933 |