| 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 | |
