Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
14
88.7
|
|
Height (m) |
0.6
3.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
57.7
925
|
|
Wingspan (Beam) (m) |
0.1
19.8
95
|
|
Weights | ||
Empty weight (kg) |
8
2,503.4
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
5,069.8
575,000
|
|
Loaded weight (kg) |
5
4,524
242,500
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
293
28,165
|
|
Сruise Speed (km/h) |
52
254
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,350
60,000
|
2 powerplants 675 hp each |
Performance | ||
Service ceiling (m) |
0.6
6,217.9
161,544
|
|
Range (Ferry range) (km) |
4
662
40,700
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
8.7
105
|
to 3050 |
Combat | ||
Guns (qt) |
1
2
18
|
.30 in (7.62 mm) machine guns |
Bombs weight (kg) |
2
544
39,000
|
bombs carried beneath fuselage |
Stat | ||
Number built (qt) |
0
14
43,000
|
|
Introduction | 1931 | |
First flight | 1931 | |
Stop production | 1939 |