Airbus A310-300 vs. lockheed C-130 hercules

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Airbus A310-300 versus lockheed C-130 hercules
46.66 m 153 ft 1 in length 29.79 m 97 ft 9 in
15.8 m 51 ft 10 in height 11.66 m 38 ft 3 in
43.9 m 144 ft wingspan 40.41 m 132 ft 7 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Allison T56-A-15 turboprop engines
52,000 lb thrust per engine Approximately 4,590 hp per engine
104,000 lb total thrust Approximately 18,360 hp total
148,768 kg 328,000 lb MTOW 70,307 kg 155,000 lb
8,050 km 4,348 nm range 3,760 km 2,031 nm
482 knots 279 mph cruise speed 540 km/h 335 mph
190-230 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.