Airbus A300-600 vs. de Havilland Venom

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Airbus A300-600 versus de Havilland Venom
54.10 m 177 ft 6 in length 6.71 m 22 ft 0 in
16.5 m 54 ft 2 in height 1.88 m 6 ft 2 in
44.84 m 147 ft 1 in wingspan 12.7 m 41 ft 8 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 (de Havilland Ghost 105)
56,000lb to 61,500lb thrust per engine 23.6 kN
112,000–123,000 lb total thrust 23.6 kN
171,700 kg 378,600 lb MTOW 6,945 kg 15,300 lb
7,500 km 4,052 nm range 1,730 km 935 nm
897 km/h 557 mph cruise speed 1030 km/h 640 mph
210-250 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.