Type | Aircraft | |
Company | Lockheed Corporation | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
10.5
88.7
|
|
Height (m) |
0.6
3.4
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
22.1
925
|
|
Wingspan (Beam) (m) |
0.1
11.8
95
|
|
Aspect ratio |
1.7
6.4
25.6
|
|
Weights | ||
Empty weight (kg) |
8
3,819.3
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
7,645.8
575,000
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
965
28,165
|
|
Power | ||
Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
Thrust (kN) |
1.5
20.5
1,914
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
14,020.8
161,544
|
|
Range (Ferry range) (km) |
4
1,930
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
1,398
36,000
|
|
Combat | ||
Guns (qt) |
1
6
18
|
0.50 in (12.7 mm) M3 Browning machine guns |
Bombs (qt) |
1
2
250
|
2 × 454 kg bombs |
Rockets (qt) |
1
8
76
|
127mm unguided rockets |
Stat | ||
Number built (qt) |
0
1,715
43,000
|
|
Price (USD) |
41.5
110,000
750.0 million
|
|
Introduction | 1945 | |
First flight | 08.01.1944 |