Lockheed Martin C-130J Super Hercules vs. Cessna 152

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Lockheed Martin C-130J Super Hercules versus Cessna 152
34.37 m 112 ft 9 in length 7.34 m 24 ft 1 in
11.86 m 38 ft 11 in height 2.59 m 8 ft 6 in
40.41 m 132 ft 7 in wingspan 10.16 m 33 ft 4 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 x Lycoming O-235-L2C flat-4 piston engine
Approximately 4,700 hp per engine thrust per engine 115 horsepower (86 kW)
Approximately 18,800 hp total total thrust 115 horsepower (86 kW)
76,610 kg 168,900 lb MTOW 757 kg 1,669 lb
4,600 km 2,485 nm range 610 km 329 nm
660 km/h 410 mph cruise speed 185 km/h 115 mph
based on configuration capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.