Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
6.8
88.7
|
|
Height (m) |
0.6
2.7
50.1
|
|
Wings | ||
Wingspan (Beam) (m) |
0.1
9.5
95
|
|
Weights | ||
Empty weight (kg) |
8
424
276,800
|
|
Loaded weight (kg) |
5
658
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
219
28,165
|
|
Сruise Speed (km/h) |
52
191
3,087
|
|
Power | ||
Total Power (hp) |
0.4
100
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
4,875
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
256
36,000
|
|
Stat | ||
Number built (qt) |
0
1
43,000
|
|
Introduction | 1945 | |
First flight | 10.12.1945 |