Airbus A321-200 vs. de Havilland Venom

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Airbus A321-200 versus de Havilland Venom
44.51 m 146 ft 0 in length 6.71 m 22 ft 0 in
11.76 m 38 ft 7 in height 1.88 m 6 ft 2 in
35.8 m 117 ft 5 in wingspan 12.7 m 41 ft 8 in
2 GE CFM56-5B3 engines 1 (de Havilland Ghost 105)
31,600 lbs thrust per engine 23.6 kN
63,200 lbs total thrust 23.6 kN
89,000 kg 196,200 lb MTOW 6,945 kg 15,300 lb
4,000 nmi 7,408 km range 1,730 km 935 nm
871 km/h 541 mph cruise speed 1030 km/h 640 mph
185 to 220 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.