North American P-51 Mustang vs. Lockheed Martin C-130J Super Hercules

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North American P-51 Mustang versus Lockheed Martin C-130J Super Hercules
9.83 m 32 ft 3 in length 34.37 m 112 ft 9 in
4.08 m 13 ft 5 in height 11.86 m 38 ft 11 in
11.28 m 37 ft wingspan 40.41 m 132 ft 7 in
Packard Rolls Royce Merlin V-1650-7 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) thrust per engine Approximately 4,700 hp per engine
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) total thrust Approximately 18,800 hp total
5,489 kg 12,100 lb MTOW 76,610 kg 168,900 lb
2,200 km 1,188 nm range 4,600 km 2,485 nm
325 mph 525 km/h cruise speed 660 km/h 410 mph
2,000 pounds of bombs, or ten 5-inch rockets 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.