Airbus A310-300 vs. Boeing CH-47 Chinook
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here.
Airbus A310-300 |
versus |
Boeing CH-47 Chinook |
46.66 m |
153 ft 1 in |
length |
15.88 m |
51 feet 2 inches |
15.8 m |
51 ft 10 in |
height |
5.68 m |
18 feet 7.8 inches |
43.9 m |
144 ft |
wingspan |
|
|
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
52,000 lb |
thrust per engine |
4,868 hp |
104,000 lb |
total thrust |
9,736 hp |
148,768 kg |
328,000 lb |
MTOW |
22,680 kg |
50,000 lb |
8,050 km |
4,348 nm |
range |
370 km |
200 nm |
482 knots |
279 mph |
cruise speed |
259 km/h |
161 mph |
190-230 passengers |
capacity |
33-55 |
|
|
rotor diameter |
18.3 m |
60 ft |
|
|
rate of climb |
10.2 m/s |
2,008 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.