Boeing 717-200HGW vs. McDonnell Douglas F-4 Phantom II

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Boeing 717-200HGW versus McDonnell Douglas F-4 Phantom II
37.80 m 123 ft 11 in length 19.2 m 63 ft 0 in
8.87 m 29 ft 1 in height 5.03 m 16 ft 6 in
28.44 m 93 ft 4 in wingspan 11.72 m 38 ft 5 in
2 Rolls-Royce BR715 engines Two General Electric J79s
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine 17,900 lbs
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust 35,800 lbs
54,885 kg 121,000 lb MTOW 27,965 kg 61,700 lb
2,060 nm 3,814 km range 3,031 km 1,636 nm
811 km/h 504 mph cruise speed Mach 2.2 2,717 km/h
106 passengers in a 2 class configuration 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.