Type | Aircraft | |
Company | Société des avions Caudron | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
7.8
88.7
|
|
Height (m) |
0.6
2.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
9
925
|
|
Wingspan (Beam) (m) |
0.1
7.7
95
|
|
Weights | ||
Empty weight (kg) |
8
672
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
1,050
575,000
|
|
Loaded weight (kg) |
5
1,050
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
pilot |
Speeds | ||
Max. Speed (km/h) |
25
370
28,165
|
|
Сruise Speed (km/h) |
52
340
3,087
|
|
Power | ||
Total Power (hp) |
0.4
220
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
9,700
161,544
|
|
Range (Ferry range) (km) |
4
1,100
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
660
36,000
|
|
Stat | ||
Number built (qt) |
0
19
43,000
|
|
Introduction | 1936 | |
First flight | 18.02.1936 |