Airbus A321-200 vs. Boeing CH-47 Chinook
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Airbus A321-200 |
versus |
Boeing CH-47 Chinook |
44.51 m |
146 ft 0 in |
length |
15.88 m |
51 feet 2 inches |
11.76 m |
38 ft 7 in |
height |
5.68 m |
18 feet 7.8 inches |
35.8 m |
117 ft 5 in |
wingspan |
|
|
2 GE CFM56-5B3 |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
31,600 lbs |
thrust per engine |
4,868 hp |
63,200 lbs |
total thrust |
9,736 hp |
89,000 kg |
196,200 lb |
MTOW |
22,680 kg |
50,000 lb |
4,000 nmi |
7,408 km |
range |
370 km |
200 nm |
871 km/h |
541 mph |
cruise speed |
259 km/h |
161 mph |
185 to 220 |
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.