| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.7
88.7
|
|
| Height (m) |
0.6
4.1
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
18.2
925
|
|
| Wingspan (Beam) (m) |
0.1
6.4
95
|
|
| Weights | ||
| Empty weight (kg) |
8
6,350
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
13,170
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Hardpoints (qt) |
1
7
2,576
|
with a capacity of 1814 kg |
| Speeds | ||
| Ground Speed (km/h) |
96.6
1,473
1,500
|
|
| Max. Speed (km/h) |
25
2,173
28,165
|
|
| Landing Speed (km/h) |
68
270
270
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
2,650
320,000
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.5
2.1
|
|
| Afterburning thrust (kN/kg) |
29.4
69
980
|
1 powerplant |
| Thrust (kN) |
1.5
48
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
15,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,368
40,700
|
|
| Dynamic Performance | ||
| Load factor from (G) |
2
7
9
|
|
| Rate of climb (m/min) |
1.9
14,640
36,000
|
|
| Combat | ||
| Guns (qt) |
1
1
18
|
20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, 725 rounds |
| Missiles (qt) |
1
4
24
|
AIM-9 Sidewinder |
| Stat | ||
| Number built (qt) |
0
2,578
43,000
|
|
| Price (USD) |
41.5
1.4 million
750.0 million
|
|
| Introduction | 20.02.1958 | |
| First flight | 17.02.1956 | |
| Stop production | 31.10.2004 | |
