Airbus A300-600 vs. Lockheed T-33 Shooting Star

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Airbus A300-600 versus Lockheed T-33 Shooting Star
54.10 m 177 ft 6 in length 11.51 m 37 ft 9 in
16.5 m 54 ft 2 in height 3.56 m 11 ft 8 in
44.84 m 147 ft 1 in wingspan 11.9 m 39 ft 1 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 (Allison J33-A-5)
56,000lb to 61,500lb thrust per engine 24.0 kN
112,000–123,000 lb total thrust 24.0 kN
171,700 kg 378,600 lb MTOW 5,900 kg 13,000 lb
7,500 km 4,052 nm range 2,050 km 1,107 nm
897 km/h 557 mph cruise speed 965 km/h 600 mph
210-250 passengers capacity 907 kg of bombs or rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.