Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
29.8
88.7
|
|
Height (m) |
0.6
11.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
162.1
925
|
|
Wingspan (Beam) (m) |
0.1
40.4
95
|
|
Weights | ||
Empty weight (kg) |
8
34,400
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
70,300
575,000
|
|
Capacity | ||
Crew (per.) |
1
5
112
|
two pilots, navigator, flight engineer and loadmaster |
Useful load (kg) |
26.4
33,000
90,700
|
|
Payload (kg) |
23
20,400
122,470
|
|
Speeds | ||
Max. Speed (km/h) |
25
592
28,165
|
at 6060 m |
Сruise Speed (km/h) |
52
540
3,087
|
|
Fuel | ||
Fuel External (l) |
142.5
10,025
10,025
|
|
Power | ||
Total Power (hp) |
0.4
18,400
60,000
|
4 powerplants 4600 hp each |
Performance | ||
Service ceiling (m) |
0.6
10,060
161,544
|
empty |
0.6
7,077
161,544
|
with 19090 kg payload | |
Range (Ferry range) (km) |
4
3,800
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
558
36,000
|
|
Stat | ||
Number built (qt) |
0
2,300
43,000
|
|
Price (USD) |
41.5
30.1 million
750.0 million
|
|
Introduction | 1954 | |
First flight | 23.08.1954 |