McDonnell-Douglas MD-11 vs. Lockheed Martin C-130J Super Hercules

versus
... or view the full comparison list here.
McDonnell-Douglas MD-11 versus Lockheed Martin C-130J Super Hercules
61.20 m 200 ft 10 in length 34.37 m 112 ft 9 in
17.6 m 57 ft 9 in height 11.86 m 38 ft 11 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 Rolls-Royce AE 2100D3 turboprop engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 4,700 hp per engine
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 18,800 hp total
285,990 kg 630,400 lb MTOW 76,610 kg 168,900 lb
13,231 km 7,147 nm range 4,600 km 2,485 nm
961 km/h 597 mph cruise speed 660 km/h 410 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.