Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Integrated Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
31.0
88.7
|
|
Height (m) |
0.6
5.6
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
17.0
95
|
|
Aspect ratio |
1.7
1.7
25.6
|
|
Weights | ||
Empty weight (kg) |
8
27,604
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
63,503
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
pilot and fire control officer |
Speeds | ||
Max. Speed (km/h) |
25
3,661
28,165
|
at 24400 |
Сruise Speed (km/h) |
52
2,125
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
46,180
320,000
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
Thrust (kN) |
1.5
182.4
1,914
|
2 powerplants 91,2 kN each |
Performance | ||
Service ceiling (m) |
0.6
27,400
161,544
|
|
Range (Ferry range) (km) |
4
4,800
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
3,600
36,000
|
|
Combat | ||
Missiles (qt) |
1
3
24
|
Hughes AIM-47A air-to-air missiles |
Stat | ||
Number built (qt) |
0
3
43,000
|
|
Price (USD) |
41.5
18.0 million
750.0 million
|
|
Introduction | 1963 | |
First flight | 07.08.1963 |