| 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 | |
