| 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 | |
