| Type | Aircraft | |
| Company | North American Aviation | |
| Scheme | Concept High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
27.2
88.7
|
|
| Height (m) |
0.6
6.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
173.3
925
|
|
| Wingspan (Beam) (m) |
0.1
17.5
95
|
|
| Wing loading (kg/m2) |
3.1
183.4
829
|
|
| Weights | ||
| Empty weight (kg) |
8
23,091.0
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
46,508
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
3,190
28,165
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.6
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
260.6
980
|
2 powerplants 130,3 |
| Thrust (kN) |
1.5
186
1,914
|
2 powerplants 93 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
24,414.5
161,544
|
|
| Range (Ferry range) (km) |
4
2,033
40,700
|
combat |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
5,486
36,000
|
|
| Combat | ||
| Guns (qt) |
1
4
18
|
20 mm cannon |
| Missiles (qt) |
1
3
24
|
Hughes GAR-9A air-to-air missiles in a rotary weapons bay |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1959 | |
