| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
27.9
88.7
|
|
| Height (m) |
0.6
8.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
92.9
925
|
|
| Wingspan (Beam) (m) |
0.1
31.7
95
|
|
| Weights | ||
| Empty weight (kg) |
8
22,650
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
36,240
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
7
112
|
or 9 |
| Speeds | ||
| Max. Speed (km/h) |
25
586
28,165
|
all engines |
| Сruise Speed (km/h) |
52
333
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
15,936.5
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
14,800
60,000
|
4 powerplants 3700 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,827
161,544
|
|
| Range (Ferry range) (km) |
4
3,540
40,700
|
|
| Combat | ||
| Rockets (qt) |
1
1
76
|
2.75 in (70 mm) FFAR in removable wing-mounted pods |
| Bombs weight (kg) |
2
3,629
39,000
|
including free-fall bombs, depth charges, and torpedoes |
| Stat | ||
| Introduction | 1945 | |
| First flight | 17.05.1945 | |
| Stop production | 1984 | |
