| 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 | |
