| 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 | |
