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 |