Airbus A310-300 vs. Lockheed C-5 Galaxy

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Airbus A310-300 versus Lockheed C-5 Galaxy
46.66 m 153 ft 1 in length 75.31 m 247 ft 2 in
15.8 m 51 ft 10 in height 19.84 m 65 ft 1 in
43.9 m 144 ft wingspan 67.89 m 222 ft 9 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x General Electric TF39 turbofan engines
52,000 lb thrust per engine 41,000 pounds of thrust (182 kilonewtons)
104,000 lb total thrust 164,000 pounds
148,768 kg 328,000 lb MTOW 381,018 kg 840,000 lb
8,050 km 4,348 nm range 8,000 km 4,320 nm
482 knots 279 mph cruise speed 908 km/h 564 mph
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.