Airbus A310-300 vs. Lockheed T-33 Shooting Star

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Airbus A310-300 versus Lockheed T-33 Shooting Star
46.66 m 153 ft 1 in length 11.51 m 37 ft 9 in
15.8 m 51 ft 10 in height 3.56 m 11 ft 8 in
43.9 m 144 ft wingspan 11.9 m 39 ft 1 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 (Allison J33-A-5)
52,000 lb thrust per engine 24.0 kN
104,000 lb total thrust 24.0 kN
148,768 kg 328,000 lb MTOW 5,900 kg 13,000 lb
8,050 km 4,348 nm range 2,050 km 1,107 nm
482 knots 279 mph cruise speed 965 km/h 600 mph
190-230 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.