Cessna O-2 Skymaster vs. lockheed C-130 hercules

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Cessna O-2 Skymaster versus lockheed C-130 hercules
8.9 m 29 ft 2 in length 29.79 m 97 ft 9 in
2.87 m 9 ft 5 in height 11.66 m 38 ft 3 in
11.58 m 38 ft wingspan 40.41 m 132 ft 7 in
Two 210-hp Continental IO-360s engines 4 x Allison T56-A-15 turboprop engines
210 hp thrust per engine Approximately 4,590 hp per engine
420 hp total thrust Approximately 18,360 hp total
5,400 lb 2,449 kg MTOW 70,307 kg 155,000 lb
1,705 km 921 nm range 3,760 km 2,031 nm
144 mph 232 km/h cruise speed 540 km/h 335 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.