| 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 | |
