Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
17.6
88.7
|
|
Height (m) |
0.6
4.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
89.7
925
|
|
Wingspan (Beam) (m) |
0.1
27.3
95
|
|
Weights | ||
Empty weight (kg) |
8
7,402.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
12,552.3
575,000
|
|
Loaded weight (kg) |
5
10,866
242,500
|
|
Capacity | ||
Crew (per.) |
1
6
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
348
28,165
|
at 3050 |
Сruise Speed (km/h) |
52
269
3,087
|
|
Power | ||
Total Power (hp) |
0.4
2,000
60,000
|
2 powerplants 1000 each |
Performance | ||
Service ceiling (m) |
0.6
7,284.7
161,544
|
|
Range (Ferry range) (km) |
4
1,450
40,700
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
9.9
105
|
to 3050 |
Combat | ||
Guns (qt) |
1
3
18
|
.30 in (7.62 mm) machine guns |
Bombs weight (kg) |
2
2,000
39,000
|
|
Stat | ||
Number built (qt) |
0
350
43,000
|
|
Price (USD) |
41.5
58,500
750.0 million
|
|
Introduction | 1935 | |
First flight | 01.04.1935 | |
Stop production | 1946 |