Type | Aircraft | |
Company | North American Aviation | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
23.3
88.7
|
|
Height (m) |
0.6
5.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
65.1
925
|
|
Wingspan (Beam) (m) |
0.1
16.2
95
|
|
Wing loading (kg/m2) |
3.1
308.3
829
|
|
Weights | ||
Empty weight (kg) |
8
14,838.8
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
28,615
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Ground Speed (km/h) |
96.6
1,107
1,500
|
|
Max. Speed (km/h) |
25
2,123
28,165
|
at 12200 m |
Fuel | ||
Fuel Capacity (l) |
23
13,625
320,000
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.7
2.1
|
|
Afterburning thrust (kN/kg) |
29.4
152
980
|
2 powerplants 76 kN each |
Thrust (kN) |
1.5
96
1,914
|
2 powerplants 48 kN each |
Performance | ||
Service ceiling (m) |
0.6
15,880.1
161,544
|
|
Range (Ferry range) (km) |
4
3,700
40,700
|
|
Сombat radius (km) |
277
2,075
7,210
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
2,438.4
36,000
|
|
Combat | ||
Guns (qt) |
1
3
18
|
1× Mark 27 nuclear bomb, B28 or B43 freefall nuclear bomb in internal weapons bay; 2× B43, Mark 83, or Mark 84 bombs on two external hardpoints |
Stat | ||
Number built (qt) |
0
156
43,000
|
|
Introduction | 1958 | |
First flight | 31.08.1958 | |
Stop production | 20.11.1979 |