Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
15.2
88.7
|
|
Height (m) |
0.6
5.6
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
21.4
95
|
|
Weights | ||
Empty weight (kg) |
8
10,364.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
15,875.7
575,000
|
|
Loaded weight (kg) |
5
12,519
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
570
28,165
|
|
Power | ||
Total Power (hp) |
0.4
4,000
60,000
|
2 powerplants 2000 each |
Performance | ||
Service ceiling (m) |
0.6
6,705.6
161,544
|
|
Range (Ferry range) (km) |
4
2,300
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
381
36,000
|
|
Combat | ||
Rockets (qt) |
1
10
76
|
5-inch (12.7 cm) HVAR rockets on "zero length" launch pylons, five under each outer wing panel |
Bombs weight (kg) |
2
2,700
39,000
|
|
Stat | ||
Number built (qt) |
0
2,452
43,000
|
|
Price (USD) |
41.5
242,595
750.0 million
|
|
Introduction | 1942 | |
First flight | 10.07.1942 | |
Stop production | 1980 |