Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
14.0
88.7
|
|
Height (m) |
0.6
6.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
56.2
925
|
|
Wingspan (Beam) (m) |
0.1
21.3
95
|
|
Weights | ||
Empty weight (kg) |
8
8,348.4
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
15,766.9
575,000
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
546
28,165
|
|
Сruise Speed (km/h) |
52
270
3,087
|
|
Power | ||
Total Power (hp) |
0.4
3,000
60,000
|
1powerplant |
Performance | ||
Service ceiling (m) |
0.6
7,467.6
161,544
|
|
Range (Ferry range) (km) |
4
2,013
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
423.7
36,000
|
|
Combat | ||
Guns (qt) |
1
7
18
|
4 × wing mounted .50 in (12.7 mm) machine guns; 2 × .50 in (12.7 mm) machine guns in dorsal turret; 1 × .50 in machine gun in ventral bath |
Torpedoes (qt) |
1
4
4
|
|
Bombs weight (kg) |
2
3,810
39,000
|
or |
Stat | ||
Number built (qt) |
0
2
43,000
|
|
Introduction | 1945 | |
First flight | 13.03.1945 |