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 |