Airbus A350-1000 vs. McDonnell Douglas F-4 Phantom II

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Airbus A350-1000 versus McDonnell Douglas F-4 Phantom II
73.79 m 242 ft 1 in length 19.2 m 63 ft 0 in
17.08 m 56 ft height 5.03 m 16 ft 6 in
64.75 m 212 ft 5 in wingspan 11.72 m 38 ft 5 in
2 Trent XWB-97 turbofan engines engines Two General Electric J79s
97,000 lb thrust per engine 17,900 lbs
194,000 lb total thrust 35,800 lbs
319,000 kg 703,300 lb MTOW 27,965 kg 61,700 lb
16,100 km 8,695 nm range 3,031 km 1,636 nm
1,099 km/h 683 mph cruise speed Mach 2.2 2,717 km/h
350 to 410 passengers capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.