| 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 | |
