| 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 | |
