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 |