| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
39.8
88.7
|
|
| Height (m) |
0.6
14.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
233.1
925
|
|
| Wingspan (Beam) (m) |
0.1
53.1
95
|
|
| Weights | ||
| Empty weight (kg) |
8
45,887.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
88,223.7
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
5
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
489
28,165
|
at 6340 |
| Сruise Speed (km/h) |
52
370
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
15,200
60,000
|
4 powerplants 3800 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,644.6
161,544
|
|
| Range (Ferry range) (km) |
4
10,975
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
231.7
36,000
|
|
| Stat | ||
| Number built (qt) |
0
448
43,000
|
|
| Introduction | 1949 | |
| First flight | 27.11.1949 | |
| Stop production | 1974 | |
