| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
19.2
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
92.9
925
|
|
| Wingspan (Beam) (m) |
0.1
31.4
95
|
|
| Aspect ratio |
1.7
10.6
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
6,486
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
18,144
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
805
28,165
|
|
| Сruise Speed (km/h) |
52
690
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
5,791.7
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
85
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
21,300
161,544
|
|
| Range (Ferry range) (km) |
4
10,308.2
40,700
|
|
| Endurance (h) |
0.0
12
150
|
|
| Stat | ||
| Number built (qt) |
0
104
43,000
|
|
| Introduction | 1955 | |
| First flight | 01.08.1955 | |
