Airbus A310-300 vs. Lockheed F-104 Starfighter

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Airbus A310-300 versus Lockheed F-104 Starfighter
46.66 m 153 ft 1 in length 16.69 m 54 ft 9 in
15.8 m 51 ft 10 in height 4.11 m 13 ft 6 in
43.9 m 144 ft wingspan 6.68 m 21 ft 11 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 Turbojet Engine
52,000 lb thrust per engine 46.7 / 71.2 kN (dry/with Afterburner)
104,000 lb total thrust 46.7 / 71.2 kN (dry/with Afterburner)
148,768 kg 328,000 lb MTOW 13,500 kg 29,800 lb
8,050 km 4,348 nm range 1,200 km 648 nm
482 knots 279 mph cruise speed 510 mph 821 km/h
190-230 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.