North American Rockwell OV-10 Bronco vs. Lockheed Martin C-130J Super Hercules

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North American Rockwell OV-10 Bronco versus Lockheed Martin C-130J Super Hercules
12.7 m 41 ft 7 in length 34.37 m 112 ft 9 in
4.62 m 15 ft 2 in height 11.86 m 38 ft 11 in
12.19 m 40 ft wingspan 40.41 m 132 ft 7 in
2 x Garrett T76-G-420/421 turboprop engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 715 hp each thrust per engine Approximately 4,700 hp per engine
Approximately 1,430 hp total total thrust Approximately 18,800 hp total
14,444 lb 6,553 kg MTOW 76,610 kg 168,900 lb
1,931 km 1,043 nm range 4,600 km 2,485 nm
244 mph 393 km/h cruise speed 660 km/h 410 mph
Pilot and observer 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.