Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
10.0
88.7
|
|
Height (m) |
0.6
3.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
9.7
925
|
|
Wingspan (Beam) (m) |
0.1
7.8
95
|
|
Wing loading (kg/m2) |
3.1
338
829
|
|
Weights | ||
Empty weight (kg) |
8
2,266
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
5,706
575,000
|
|
Loaded weight (kg) |
5
3,266
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
833
28,165
|
at 3048 |
Сruise Speed (km/h) |
52
628
3,087
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.0
2.1
|
|
Thrust (kN) |
1.5
30
1,914
|
2 powerplants 15 kN each |
Performance | ||
Service ceiling (m) |
0.6
12,400
161,544
|
|
Range (Ferry range) (km) |
4
965
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
3,660
36,000
|
|
Stat | ||
Number built (qt) |
0
2
43,000
|
|
Introduction | 1962 | |
First flight | 07.07.1962 |