North American B-25 Mitchell vs. lockheed C-130 hercules

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North American B-25 Mitchell versus lockheed C-130 hercules
16.15 m 53 ft 0 in length 29.79 m 97 ft 9 in
5 m 16 ft 4 in height 11.66 m 38 ft 3 in
20.58 m 67 ft 6 in wingspan 40.41 m 132 ft 7 in
2 x Wright R-2600-92 Twin Cyclone engines 4 x Allison T56-A-15 turboprop engines
1,700 horsepower thrust per engine Approximately 4,590 hp per engine
3,400 horsepower total thrust Approximately 18,360 hp total
7,484 kg 16,500 lb MTOW 70,307 kg 155,000 lb
1,350 mi 1,175 nm range 3,760 km 2,031 nm
233 MPH 375 km/h cruise speed 540 km/h 335 mph
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.