Sukhoi SSJ 100 95LR vs. McDonnell Douglas F-4 Phantom II

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Sukhoi SSJ 100 95LR versus McDonnell Douglas F-4 Phantom II
29.94 m 98 ft 2 in length 19.2 m 63 ft 0 in
10.28 m 33 ft 8 in height 5.03 m 16 ft 6 in
27.8 m 91 ft 2 in wingspan 11.72 m 38 ft 5 in
2 PowerJet SaM146 turbofans engines Two General Electric J79s
15,400 (68.5 KN) to 16,100 (71.6 KN) at NTO, 17,500 (77.9 KN) to 17,800 (79.2 KN) with APR thrust per engine 17,900 lbs
30,800 (137 KN) to 32,200 (143.2 KN) at NTO, 35,000 (155.8 KN) to 35,600 (158.4 KN) with APR total thrust 35,800 lbs
49,450 kg 109,000 lb MTOW 27,965 kg 61,700 lb
4,578 km 2,470 nm range 3,031 km 1,636 nm
515 mph 830 km/h cruise speed Mach 2.2 2,717 km/h
98 (up to 108) 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.