| Company | Société des avions Caudron | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.6
88.7
|
|
| Height (m) |
0.6
3.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
65
925
|
|
| Wingspan (Beam) (m) |
0.1
17
95
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Empty weight (kg) |
8
1,300
276,800
|
|
| Loaded weight (kg) |
5
2,100
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
150
28,165
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
485.4
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
240
60,000
|
3 powerplants 80 hp each |
| Performance | ||
| Endurance (h) |
0.0
5
150
|
|
| Propellers | ||
| Prop blade number (qt) |
1
2
8
|
|
| Stat | ||
| First flight | 1920 | |
