| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
35.4
88.7
|
|
| Height (m) |
0.6
7.5
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
153.7
925
|
|
| Wingspan (Beam) (m) |
0.1
38.5
95
|
|
| Wing loading (kg/m2) |
3.1
428
829
|
|
| Weights | ||
| Empty weight (kg) |
8
36,151.3
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
62,369.0
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
5
112
|
flight crew |
| Useful load (kg) |
26.4
29,620
90,700
|
|
| Capacity passengers (per.) |
1
95
400
|
109 in high-density configuration |
| Speeds | ||
| Max. Speed (km/h) |
25
607
28,165
|
|
| Сruise Speed (km/h) |
52
547
3,087
|
at 6890 m |
| Stall Speed (km/h) |
40
160
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
17,755
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
13,000
60,000
|
4 powerplants 3250 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
7,620
161,544
|
|
| Range (Ferry range) (km) |
4
8,700
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
493.8
36,000
|
|
| Stat | ||
| Number built (qt) |
0
856
43,000
|
|
| Introduction | 1943 | |
| First flight | 09.01.1943 | |
| Stop production | 1990 | |
