Cessna O-2 Skymaster vs. Lockheed Martin C-130J Super Hercules

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Cessna O-2 Skymaster versus Lockheed Martin C-130J Super Hercules
8.9 m 29 ft 2 in length 34.37 m 112 ft 9 in
2.87 m 9 ft 5 in height 11.86 m 38 ft 11 in
11.58 m 38 ft wingspan 40.41 m 132 ft 7 in
Two 210-hp Continental IO-360s engines 4 x Rolls-Royce AE 2100D3 turboprop engines
210 hp thrust per engine Approximately 4,700 hp per engine
420 hp total thrust Approximately 18,800 hp total
5,400 lb 2,449 kg MTOW 76,610 kg 168,900 lb
1,705 km 921 nm range 4,600 km 2,485 nm
144 mph 232 km/h cruise speed 660 km/h 410 mph
2 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.