Company | Société des avions Caudron | |
Geometry | ||
---|---|---|
Length (m) |
1.9
14.6
88.7
|
|
Height (m) |
0.6
4.8
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
70
925
|
|
Wingspan (Beam) (m) |
0.1
24.5
95
|
|
Rotors | ||
Rotor number (qt) |
1
2
8
|
|
Weights | ||
Empty weight (kg) |
8
2,690
276,800
|
|
Loaded weight (kg) |
5
4,500
242,500
|
|
Speeds | ||
Max. Speed (km/h) |
25
225
28,165
|
|
Fuel | ||
Fuel Capacity (l) |
23
901.5
320,000
|
|
Power | ||
Total Power (hp) |
0.4
900
60,000
|
3 powerplants 300 hp each |
Performance | ||
Service ceiling (m) |
0.6
7,000
161,544
|
|
Range (Ferry range) (km) |
4
2,400
40,700
|
|
Propellers | ||
Prop blade number (qt) |
1
2
8
|
|
Stat | ||
Number built (qt) |
0
1
43,000
|
|
First flight | 1930 |