Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
8.3
88.7
|
|
Height (m) |
0.6
2.8
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
27.3
925
|
|
Weights | ||
Empty weight (kg) |
8
1,945.5
276,800
|
|
Loaded weight (kg) |
5
3,220.1
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
298
28,165
|
|
Сruise Speed (km/h) |
52
241.4
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
1,574.7
320,000
|
|
Performance | ||
Service ceiling (m) |
0.6
7,955
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
390
36,000
|
|
Stat | ||
Introduction | 1929 | |
First flight | 1929 |