Lockheed U-2 vs. Lockheed Martin C-130J Super Hercules

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Lockheed U-2 versus Lockheed Martin C-130J Super Hercules
19.2 m 63 ft 0 in length 34.37 m 112 ft 9 in
4.8 m 15 ft 9 in height 11.86 m 38 ft 11 in
32 m 105 ft wingspan 40.41 m 132 ft 7 in
1 × General Electric F118-101 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
17,000 lbf (76 kN) thrust per engine Approximately 4,700 hp per engine
17,000 lbf (76 kN) total thrust Approximately 18,800 hp total
18,144 kg 40,000 lb MTOW 76,610 kg 168,900 lb
6,090 nm 11,278 km range 4,600 km 2,485 nm
475 mph 764 km/h cruise speed 660 km/h 410 mph
capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.