Company | Société des avions Caudron | |
Geometry | ||
---|---|---|
Length (m) |
1.9
12.6
88.7
|
|
Height (m) |
0.6
5.1
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
88.8
925
|
|
Wingspan (Beam) (m) |
0.1
20.9
95
|
|
Rotors | ||
Rotor number (qt) |
1
2
8
|
|
Weights | ||
Empty weight (kg) |
8
1,900
276,800
|
|
Loaded weight (kg) |
5
3,240
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
140
28,165
|
|
Сruise Speed (km/h) |
52
120
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
832.2
320,000
|
including oil |
Power | ||
Total Power (hp) |
0.4
400
60,000
|
5 powerplants 80 hp each |
Dynamic Performance | ||
Time to altitude (min) |
0.6
42
105
|
to 3000 m |
Propellers | ||
Prop blade number (qt) |
1
2
8
|
|
Stat | ||
Number built (qt) |
0
1
43,000
|
|
First flight | 1919 |