Airbus A310-300 vs. Lockheed C-5 Galaxy
... or view the full comparison list
here.
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.