Type | Aircraft | |
Company | Douglas Aircraft Company | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
13.8
88.7
|
|
Height (m) |
0.6
4.0
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
51.7
925
|
|
Wingspan (Beam) (m) |
0.1
10.2
95
|
|
Weights | ||
Empty weight (kg) |
8
7,268.4
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
12,299.6
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
1,162
28,165
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.7
2.1
|
|
Afterburning thrust (kN/kg) |
29.4
71
980
|
1 powerplant |
Thrust (kN) |
1.5
45
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
17,000
161,544
|
|
Range (Ferry range) (km) |
4
1,100
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
5,577.8
36,000
|
|
Combat | ||
Guns (qt) |
1
4
18
|
20 mm Colt Mk 12 cannon |
Missiles (qt) |
1
4
24
|
AIM-9 Sidewinder air-to-air missiles |
Rockets (qt) |
1
4
76
|
pods of 19 2.75 in (70 mm) unguided rockets |
1
6
76
|
pods of 7 2.75 in (70 mm) unguided rockets or | |
Bombs weight (kg) |
2
907
39,000
|
bombs |
Stat | ||
Number built (qt) |
0
422
43,000
|
|
Introduction | 1951 | |
First flight | 23.01.1951 | |
Stop production | 1964 |