Lockheed U-2 vs. McDonnell Douglas A-4 Skyhawk
... or view the full comparison list
here.
Lockheed U-2 |
versus |
McDonnell Douglas A-4 Skyhawk |
19.2 m |
63 ft 0 in |
length |
12.19 m |
40 ft 0 in |
4.8 m |
15 ft 9 in |
height |
4.57 m |
15 ft |
32 m |
105 ft |
wingspan |
8.08 m |
26 ft 6 in |
1 × General Electric F118-101 |
engines |
1x Pratt & Whitney J52-P-6A Jet |
17,000 lbf (76 kN) |
thrust per engine |
8,500 pound-force |
17,000 lbf (76 kN) |
total thrust |
8,500 pound-force |
18,144 kg |
40,000 lb |
MTOW |
11,113 kg |
24,500 lb |
6,090 nm |
11,278 km |
range |
3,222 km |
1,739 nm |
475 mph |
764 km/h |
cruise speed |
586 kts |
364 mph |
|
capacity |
Up to 9,155 pounds of weapons on 5 hardpoints |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.