| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
48
88.7
|
|
| Height (m) |
0.6
14.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
248.3
925
|
|
| Wingspan (Beam) (m) |
0.1
54.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
49,630.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
129,727.4
575,000
|
|
| Loaded weight (kg) |
5
125,000
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
6
112
|
two pilots, navigator, two flight engineers, loadmaster |
| Payload (kg) |
23
50,000
122,470
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
578
28,165
|
|
| Сruise Speed (km/h) |
52
519
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
30,000
60,000
|
4 powerplants 7500 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
9,845.0
161,544
|
|
| Range (Ferry range) (km) |
4
6,593.1
40,700
|
with 23587 kg payload |
| Stat | ||
| Number built (qt) |
0
50
43,000
|
|
| Introduction | 1956 | |
| First flight | 23.04.1956 | |
| Stop production | 1971 | |
