| Type | Aircraft | |
| Company | North American Aviation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
15.2
88.7
|
|
| Height (m) |
0.6
5.0
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
37
925
|
|
| Wingspan (Beam) (m) |
0.1
11.8
95
|
|
| Wing loading (kg/m2) |
3.1
352
829
|
|
| Weights | ||
| Empty weight (kg) |
8
9,500
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
15,799.5
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,390
28,165
|
|
| Сruise Speed (km/h) |
52
966
3,087
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
71
980
|
1 powerplant |
| Thrust (kN) |
1.5
45
1,914
|
|
| Performance | ||
| Service ceiling (m) |
0.6
15,240
161,544
|
|
| Range (Ferry range) (km) |
4
3,210
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
6,827.5
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
20 mm (0.787 in) Pontiac M39A1 revolver cannon |
| Missiles (qt) |
1
4
24
|
AIM-9 Sidewinder or 2 x AGM-12 Bullpup |
| Bombs weight (kg) |
2
3,190
39,000
|
|
| Stat | ||
| Number built (qt) |
0
2,294
43,000
|
|
| Price (USD) |
41.5
697,029
750.0 million
|
|
| Introduction | 1953 | |
| First flight | 25.05.1953 | |
| Stop production | 1979 | |
