| Company | Société des avions Caudron | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.6
88.7
|
|
| Height (m) |
0.6
3.0
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
17.2
95
|
|
| Weights | ||
| Empty weight (kg) |
8
940
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,435
575,000
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
150
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
260
60,000
|
2 powerplants 130 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
4,725
161,544
|
|
| Endurance (h) |
0.0
2.5
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
264
36,000
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
.303 Lewis guns |
| Bombs weight (kg) |
2
100
39,000
|
of bombs carried externally |
| Stat | ||
| Number built (qt) |
0
512
43,000
|
|
| First flight | 1916 | |
