| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.8
88.7
|
|
| Height (m) |
0.6
4.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
37.2
925
|
|
| Wingspan (Beam) (m) |
0.1
15.3
95
|
|
| Wing loading (kg/m2) |
3.1
220
829
|
|
| Weights | ||
| Empty weight (kg) |
8
5,428.6
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
11,339.8
575,000
|
|
| Loaded weight (kg) |
5
8,213
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
15
2,576
|
external hardpoints |
| Speeds | ||
| Max. Speed (km/h) |
25
518
28,165
|
at 5500 m |
| Сruise Speed (km/h) |
52
319
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
2,681.0
60,000
|
|
|
0.4
2,700
60,000
|
1 powerplant | |
| Performance | ||
| Service ceiling (m) |
0.6
8,686.8
161,544
|
|
| Range (Ferry range) (km) |
4
2,115
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
870
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
20 mm (0.79 in) M2 cannon |
| Stat | ||
| Number built (qt) |
0
3,180
43,000
|
|
| Introduction | 1949 | |
| First flight | 18.03.1945 | |
| Stop production | 1985 | |
