| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
34.6
88.7
|
|
| Height (m) |
0.6
7.5
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
154.4
925
|
|
| Wingspan (Beam) (m) |
0.1
37.5
95
|
|
| Aspect ratio |
1.7
9.2
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
31,297.9
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
54,431.1
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
|
| Capacity passengers (per.) |
1
106
400
|
47-106 Passengers |
| Speeds | ||
| Max. Speed (km/h) |
25
531
28,165
|
|
| Сruise Speed (km/h) |
52
489
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
29,337
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
13,000
60,000
|
4 powerplants 3250 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
7,833.4
161,544
|
|
| Range (Ferry range) (km) |
4
8,288
40,700
|
|
| Stat | ||
| Number built (qt) |
0
259
43,000
|
|
| Introduction | 15.12.1951 | |
| First flight | 14.07.1951 | |
