Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
15.2
88.7
|
|
Height (m) |
0.6
3.6
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
20.0
95
|
|
Weights | ||
Empty weight (kg) |
8
5,670
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
9,825
575,000
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Capacity passengers (per.) |
1
18
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
428
28,165
|
at 5230 m |
Power | ||
Total Power (hp) |
0.4
2,400
60,000
|
2 powerplants 1200 hp each |
Performance | ||
Service ceiling (m) |
0.6
7,740
161,544
|
|
Range (Ferry range) (km) |
4
4,025
40,700
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
6.6
105
|
to 3050 m |
Stat | ||
Number built (qt) |
0
625
43,000
|
|
Introduction | 1953 | |
First flight | 21.09.1939 |