Airbus A310-300 vs. Lockheed Martin F-22 Raptor

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Airbus A310-300 versus Lockheed Martin F-22 Raptor
46.66 m 153 ft 1 in length 18.9 m 62 ft 1 in
15.8 m 51 ft 10 in height 5.1 m 16 ft 9 in
43.9 m 144 ft wingspan 13.6 m 44 ft 7 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Two Pratt & Whitney F119-PW-100 turbofan engines
52,000 lb thrust per engine 35,000-pound class
104,000 lb total thrust 70,000-pound class
148,768 kg 328,000 lb MTOW 38,000 kg 83,500 lb
8,050 km 4,348 nm range 1,850 mi 1,611 nm
482 knots 279 mph cruise speed Mach 1.6 1976 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.