Lockheed U-2 vs. lockheed C-130 hercules

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Lockheed U-2 versus lockheed C-130 hercules
19.2 m 63 ft 0 in length 29.79 m 97 ft 9 in
4.8 m 15 ft 9 in height 11.66 m 38 ft 3 in
32 m 105 ft wingspan 40.41 m 132 ft 7 in
1 × General Electric F118-101 engines 4 x Allison T56-A-15 turboprop engines
17,000 lbf (76 kN) thrust per engine Approximately 4,590 hp per engine
17,000 lbf (76 kN) total thrust Approximately 18,360 hp total
18,144 kg 40,000 lb MTOW 70,307 kg 155,000 lb
6,090 nm 11,278 km range 3,760 km 2,031 nm
475 mph 764 km/h cruise speed 540 km/h 335 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.