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 |