| Company | Société des avions Caudron | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
13
88.7
|
|
| Height (m) |
0.6
3.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
107
925
|
|
| Rotors | ||
| Rotor number (qt) |
1
2
8
|
|
| Weights | ||
| Empty weight (kg) |
8
2,341
276,800
|
|
| Loaded weight (kg) |
5
4,170
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
143
28,165
|
|
| Stall Speed (km/h) |
40
82.2
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
980
320,000
|
and 132 l |
| Power | ||
| Total Power (hp) |
0.4
520
60,000
|
2 powerplants 260 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
3,500
161,544
|
|
| Endurance (h) |
0.0
6.8
150
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
41
105
|
to 4000 m |
| Propellers | ||
| Prop blade number (qt) |
1
2
8
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
a pair of Lewis guns in nose and mid-upper positions |
| Bombs weight (kg) |
2
600
39,000
|
|
| Stat | ||
| Number built (qt) |
0
54
43,000
|
|
| First flight | 01.02.1918 | |
