Type | Aircraft | |
Company | North American Aviation | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
21.4
88.7
|
|
Height (m) |
0.6
7.4
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
77.8
925
|
|
Wingspan (Beam) (m) |
0.1
21.8
95
|
|
Wing loading (kg/m2) |
3.1
274
829
|
|
Weights | ||
Empty weight (kg) |
8
16,034.5
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
27,759.9
575,000
|
|
Loaded weight (kg) |
5
21,269
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
726
28,165
|
|
Сruise Speed (km/h) |
52
640
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
9,961
320,000
|
|
Power | ||
Total Power (hp) |
0.4
10,070
60,000
|
2 powerplants 5035 hp each |
Performance | ||
Service ceiling (m) |
0.6
11,430
161,544
|
|
Range (Ferry range) (km) |
4
3,508
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
2,078.7
36,000
|
|
Combat | ||
Guns (qt) |
1
2
18
|
20 mm cannons in tail (never fitted) |
Bombs weight (kg) |
2
4,763
39,000
|
|
Stat | ||
Introduction | 1952 | |
First flight | 04.01.1952 |