Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.1
88.7
|
|
Height (m) |
0.6
3.0
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
32.7
925
|
|
Wingspan (Beam) (m) |
0.1
15.1
95
|
|
Wing loading (kg/m2) |
3.1
120
829
|
|
Weights | ||
Empty weight (kg) |
8
2,615.0
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
4,173.1
575,000
|
|
Loaded weight (kg) |
5
3,924
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
pilot and co-pilot |
Capacity passengers (per.) |
1
6
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
362
28,165
|
at 1500 m |
Сruise Speed (km/h) |
52
341
3,087
|
|
Power | ||
Total Power (hp) |
0.4
900
60,000
|
2 powerplants 450 hp each |
Performance | ||
Service ceiling (m) |
0.6
6,979.9
161,544
|
|
Range (Ferry range) (km) |
4
1,300
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
427
36,000
|
|
Propellers | ||
Propellers (qt) |
1
2
8
|
1 per engine |
Prop diameter (m) |
1.8
2.8
5.8
|
2,6 to 2,75 m |
Prop blade number (qt) |
1
2
8
|
|
Stat | ||
Number built (qt) |
0
130
43,000
|
|
Introduction | 1936 | |
First flight | 27.06.1936 |