| Company | Société des avions Caudron | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.3
88.7
|
|
| Wings | ||
| Wing area (m2) |
1.1
30
925
|
|
| Wingspan (Beam) (m) |
0.1
10.6
95
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Loaded weight (kg) |
5
400
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
85
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
60
60,000
|
1 powerplant |
| Propellers | ||
| Prop blade number (qt) |
1
2
8
|
|
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| First flight | 01.07.1911 | |
