McDonnell-Douglas DC-9-30 vs. lockheed C-130 hercules

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McDonnell-Douglas DC-9-30 versus lockheed C-130 hercules
36.36 m 119 ft 3 in length 29.79 m 97 ft 9 in
8.5 m 27 ft 11 in height 11.66 m 38 ft 3 in
28.44 m 93 ft 4 in wingspan 40.41 m 132 ft 7 in
2x Pratt & Whitney JT8D engines 4 x Allison T56-A-15 turboprop engines
15,000 pound-force thrust per engine Approximately 4,590 hp per engine
30,000 pound-force (2 engines) total thrust Approximately 18,360 hp total
54,885 kg 121,000 lb MTOW 70,307 kg 155,000 lb
2,632 km 1,422 nm range 3,760 km 2,031 nm
898 km/h 558 mph cruise speed 540 km/h 335 mph
Up to 139 passengers 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.