Embraer E175-E2 vs. McDonnell Douglas F-4 Phantom II

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Embraer E175-E2 versus McDonnell Douglas F-4 Phantom II
29.94 m 98 ft 2 in length 19.2 m 63 ft 0 in
9.81 m 32 ft 2 in height 5.03 m 16 ft 6 in
28.7 m 94 ft 2 in wingspan 11.72 m 38 ft 5 in
2 (Pratt & Whitney Pure Power Geared Turbofan engines) engines Two General Electric J79s
67 kN thrust per engine 17,900 lbs
134 kN total thrust 35,800 lbs
44,800 kg 98,800 lb MTOW 27,965 kg 61,700 lb
3,815 km 2,060 nm range 3,031 km 1,636 nm
M 0.82 101,3 km/h cruise speed Mach 2.2 2,717 km/h
Three classes configuration: 80 seats (12 at 36”, 16 at 34”, 52 at 30”); Single class configuration: 88 seats at 31” or 90 seats (50 at 30”, 40 at 29”) 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.