McDonnell-Douglas MD-11 vs. lockheed C-130 hercules

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McDonnell-Douglas MD-11 versus lockheed C-130 hercules
61.20 m 200 ft 10 in length 29.79 m 97 ft 9 in
17.6 m 57 ft 9 in height 11.66 m 38 ft 3 in
51.6 m 169 ft 4 in wingspan 40.41 m 132 ft 7 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 4 x Allison T56-A-15 turboprop engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 4,590 hp per engine
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 18,360 hp total
285,990 kg 630,400 lb MTOW 70,307 kg 155,000 lb
13,231 km 7,147 nm range 3,760 km 2,031 nm
961 km/h 597 mph cruise speed 540 km/h 335 mph
Max 410 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.