Type | Aircraft | |
Company | Consolidated Aircraft Corporation | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
20.2
88.7
|
|
Height (m) |
0.6
5.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
97.4
925
|
|
Wingspan (Beam) (m) |
0.1
33.5
95
|
|
Weights | ||
Empty weight (kg) |
8
13,900
276,800
|
|
Loaded weight (kg) |
5
25,401
242,500
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
pilot, co-pilot, navigator, radio operator |
Capacity passengers (per.) |
1
25
400
|
or 2,700 kg of cargo for transatlantic flights and 4,500 kg max for shorter flights |
Speeds | ||
Max. Speed (km/h) |
25
483
28,165
|
at 7600 m |
Сruise Speed (km/h) |
52
346
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
11,000
320,000
|
|
Power | ||
Total Power (hp) |
0.4
4,800
60,000
|
4 powerplants 1200 hp each |
Performance | ||
Service ceiling (m) |
0.6
8,534
161,544
|
at 25000 kg take-off weight |
Range (Ferry range) (km) |
4
2,253
40,700
|
at 60% power |
Dynamic Performance | ||
Time to altitude (min) |
0.6
60
105
|
to 6100 m |
Stat | ||
Number built (qt) |
0
287
43,000
|
|
Introduction | 1942 |