Airbus A300-600 vs. North American F-100 Super Sabre

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Airbus A300-600 versus North American F-100 Super Sabre
54.10 m 177 ft 6 in length 16.46 m 54 ft 2 in
16.5 m 54 ft 2 in height 4.93 m 16 ft 2 in
44.84 m 147 ft 1 in wingspan 11.84 m 38 ft 1
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 Pratt & Whitney J57-P-21A
56,000lb to 61,500lb thrust per engine 16,000 lb. thrust in afterburner
112,000–123,000 lb total thrust 16,000 lb. (afterburner)
171,700 kg 378,600 lb MTOW 17,609 kg 38,800 lb
7,500 km 4,052 nm range 2,673 km 1,444 nm
897 km/h 557 mph cruise speed 587 mph 945 km/h
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.