Type | Aircraft | |
Company | Consolidated Aircraft Corporation | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
25.0
88.7
|
|
Height (m) |
0.6
9.8
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
132.1
925
|
|
Wingspan (Beam) (m) |
0.1
41.2
95
|
|
Weights | ||
Empty weight (kg) |
8
27,341.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
55,905.3
575,000
|
|
Loaded weight (kg) |
5
45,800
242,500
|
|
Capacity | ||
Crew (per.) |
1
10
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
575
28,165
|
at 9150 |
Сruise Speed (km/h) |
52
467
3,087
|
|
Power | ||
Total Power (hp) |
0.4
8,800
60,000
|
4 powerplants 2200 hp each |
Performance | ||
Service ceiling (m) |
0.6
9,357.4
161,544
|
|
Range (Ferry range) (km) |
4
6,118
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
320.0
36,000
|
|
Combat | ||
Guns (qt) |
1
10
18
|
.50 in (12.7 mm) machine guns |
Bombs weight (kg) |
2
9,100
39,000
|
|
Stat | ||
Number built (qt) |
0
118
43,000
|
|
Introduction | 1942 | |
First flight | 07.09.1942 | |
Stop production | 30.08.1945 |