Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
23.3
88.7
|
|
Height (m) |
0.6
7.0
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
75.4
925
|
|
Wingspan (Beam) (m) |
0.1
22.1
95
|
|
Wing loading (kg/m2) |
3.1
421
829
|
|
Weights | ||
Empty weight (kg) |
8
17,875.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
37,194.6
575,000
|
|
Loaded weight (kg) |
5
31,750
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
982
28,165
|
at 3050 m |
Сruise Speed (km/h) |
52
837
3,087
|
|
Power | ||
Afterburning thrust (kN/kg) |
29.4
110.6
980
|
2 powerplants 55,3 kN each |
Thrust (kN) |
1.5
46.7
1,914
|
2 powerplants 46,7 kN each |
Performance | ||
Service ceiling (m) |
0.6
12,495
161,544
|
|
Range (Ferry range) (km) |
4
3,380
40,700
|
|
Combat | ||
Guns (qt) |
1
2
18
|
20 mm M3L cannon in the tail turret |
Bombs weight (kg) |
2
5,800
39,000
|
of free-fall bombs or mines |
Stat | ||
Number built (qt) |
0
282
43,000
|
|
Introduction | 1952 | |
First flight | 28.10.1952 | |
Stop production | 27.09.1991 |