| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
35.4
88.7
|
|
| Height (m) |
0.6
7.8
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
57.9
95
|
35,839 m - 57,912 m |
| Weights | ||
| Empty weight (kg) |
8
23,132.8
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
61,688.6
575,000
|
|
| Capacity | ||
| Useful load (kg) |
26.4
10,981.5
90,700
|
|
| Payload (kg) |
23
10,981.5
122,470
|
|
| Capacity passengers (per.) |
1
106
400
|
87-106 Passengers (Passenger configuration); 73 Stretcher Cases (Medical configuration) |
| Speeds | ||
| Max. Speed (km/h) |
25
770.9
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
12,193.0
60,000
|
4 powerplants 5530 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
8,046.7
161,544
|
with takeoff weight and normal power |
|
0.6
10,027
161,544
|
with combat weight and maximum power | |
| Range (Ferry range) (km) |
4
3,700.3
40,700
|
with 10981,47 kg payload |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
704.1
36,000
|
with takeoff weight and normal power |
|
1.9
1,402
36,000
|
with combat weight and maximum power | |
| Propellers | ||
| Propellers (qt) |
1
4
8
|
1 per engine |
| Prop diameter (m) |
1.8
4.6
5.8
|
|
| Prop blade number (qt) |
1
3
8
|
3 per engine |
| Stat | ||
| Number built (qt) |
0
4
43,000
|
|
| First flight | 01.09.1954 | |
