Type | Aircraft | |
Company | North American Aviation | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
18.9
88.7
|
|
Height (m) |
0.6
5.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
35
925
|
|
Wingspan (Beam) (m) |
0.1
11.2
95
|
|
Wing loading (kg/m2) |
3.1
516
829
|
|
Weights | ||
Empty weight (kg) |
8
10,294.7
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
18,840.9
575,000
|
|
Loaded weight (kg) |
5
18,033
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
2,448
28,165
|
|
Сruise Speed (km/h) |
52
965
3,087
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
Thrust (kN) |
1.5
109
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
16,215.4
161,544
|
|
Range (Ferry range) (km) |
4
3,885
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
12,161.5
36,000
|
|
Combat | ||
Bombs weight (kg) |
2
4,500
39,000
|
|
Stat | ||
Number built (qt) |
0
3
43,000
|
|
Introduction | 1956 | |
First flight | 10.09.1956 | |
Stop production | 25.11.1957 |