Airbus A300-600 vs. Boeing CH-47 Chinook
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Airbus A300-600 |
versus |
Boeing CH-47 Chinook |
54.10 m |
177 ft 6 in |
length |
15.88 m |
51 feet 2 inches |
16.5 m |
54 ft 2 in |
height |
5.68 m |
18 feet 7.8 inches |
44.84 m |
147 ft 1 in |
wingspan |
|
|
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
56,000lb to 61,500lb |
thrust per engine |
4,868 hp |
112,000–123,000 lb |
total thrust |
9,736 hp |
171,700 kg |
378,600 lb |
MTOW |
22,680 kg |
50,000 lb |
7,500 km |
4,052 nm |
range |
370 km |
200 nm |
897 km/h |
557 mph |
cruise speed |
259 km/h |
161 mph |
210-250 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.