North American T-6 Texan vs. Lockheed Martin C-130J Super Hercules

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North American T-6 Texan versus Lockheed Martin C-130J Super Hercules
9.0 m 29 ft 6 in length 34.37 m 112 ft 9 in
3.56 m 11 ft 8 in height 11.86 m 38 ft 11 in
12.8 m 42 ft wingspan 40.41 m 132 ft 7 in
1 x Pratt & Whitney R-1340-AN-1 radial engine engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 600 hp thrust per engine Approximately 4,700 hp per engine
Approximately 600 hp total thrust Approximately 18,800 hp total
5,617 lb 2,548 kg MTOW 76,610 kg 168,900 lb
1,175 km 634 nm range 4,600 km 2,485 nm
145 mph 233 km/h cruise speed 660 km/h 410 mph
Pilot and one passenger 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.