Type | Aircraft | |
Company | Caproni | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.7
88.7
|
|
Height (m) |
0.6
3.2
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
38.5
925
|
|
Wingspan (Beam) (m) |
0.1
16.4
95
|
|
Weights | ||
Empty weight (kg) |
8
4,599.4
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
6,850
575,000
|
|
Loaded weight (kg) |
5
6,800.3
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Hardpoints (qt) |
1
2
2,576
|
for 2 bombs or underwing tanks |
Speeds | ||
Ground Speed (km/h) |
96.6
410
1,500
|
|
Max. Speed (km/h) |
25
505.3
28,165
|
|
Сruise Speed (km/h) |
52
450
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,680
60,000
|
2 powerplants 840 hp each |
Performance | ||
Service ceiling (m) |
0.6
8,100
161,544
|
|
Range (Ferry range) (km) |
4
1,580
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
420
36,000
|
|
Time to altitude (min) |
0.6
9.6
105
|
to 3999 m |
Combat | ||
Bombs weight (kg) |
2
1,100
39,000
|
1000 kg in bomb bay and 100 on hardpoints |
Stat | ||
Number built (qt) |
0
3
43,000
|
|
Introduction | 1940 | |
First flight | 31.08.1940 |