Airbus A320-200 vs. Lockheed F-104 Starfighter

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Airbus A320-200 versus Lockheed F-104 Starfighter
38.7 m 127 ft 0 in length 16.69 m 54 ft 9 in
17.4 m 57 ft 1 in height 4.11 m 13 ft 6 in
35.8 m 117 ft 5 in wingspan 6.68 m 21 ft 11 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 Turbojet Engine
Between 21,000 - 33,000 lbf thrust per engine 46.7 / 71.2 kN (dry/with Afterburner)
Between 42,000 - 66,000 lbf total thrust 46.7 / 71.2 kN (dry/with Afterburner)
77,000 kg 169,800 lb MTOW 13,500 kg 29,800 lb
5,700 km 3,078 nm range 1,200 km 648 nm
530 mph 853 km/h cruise speed 510 mph 821 km/h
Typically between 140-180 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.