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 |