McDonnell Douglas F-4 Phantom II vs. Sukhoi Su-57

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McDonnell Douglas F-4 Phantom II versus Sukhoi Su-57
19.2 m 63 ft 0 in length 20.1 m 65 ft 11 in
5.03 m 16 ft 6 in height 3.8 m 12 ft 6 in
11.72 m 38 ft 5 in wingspan 14.1 m 46 ft 3 in
Two General Electric J79s engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
17,900 lbs thrust per engine 107.9 kN dry and 166.8 kN after burning
35,800 lbs total thrust 215.8 kN dry and 333.6 kN after burning
27,965 kg 61,700 lb MTOW 35,000 kg 77,200 lb
3,031 km 1,636 nm range 3,500 km 1,890 nm
Mach 2.2 2,717 km/h cruise speed Mach 2 2470 km/h
Up to 16,000 lbs of externally carried ordnance 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.