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 |