Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
35.1
88.7
|
|
Height (m) |
0.6
7.5
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
171.9
925
|
|
Wingspan (Beam) (m) |
0.1
45.7
95
|
|
Weights | ||
Empty weight (kg) |
8
45,569
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
70,807.6
575,000
|
|
Capacity | ||
Crew (per.) |
1
5
112
|
|
Capacity passengers (per.) |
1
99
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
607
28,165
|
|
Сruise Speed (km/h) |
52
467
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
37,264
320,000
|
|
Power | ||
Total Power (hp) |
0.4
13,600
60,000
|
4 powerplants 3400 hp each |
Performance | ||
Service ceiling (m) |
0.6
7,225
161,544
|
|
Range (Ferry range) (km) |
4
7,950
40,700
|
7950-9945 km |
Propellers | ||
Propellers (qt) |
1
4
8
|
1 per engine |
Prop diameter (m) |
1.8
5.8
5.8
|
|
Prop blade number (qt) |
1
3
8
|
3 per engine |
Stat | ||
Number built (qt) |
0
44
43,000
|
|
Price (USD) |
41.5
3.0 million
750.0 million
|
|
Introduction | 01.06.1957 | |
First flight | 10.10.1956 | |
Stop production | 1980 |