Sukhoi SSJ 100 95LR vs. McDonnell Douglas A-4 Skyhawk

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Sukhoi SSJ 100 95LR versus McDonnell Douglas A-4 Skyhawk
29.94 m 98 ft 2 in length 12.19 m 40 ft 0 in
10.28 m 33 ft 8 in height 4.57 m 15 ft
27.8 m 91 ft 2 in wingspan 8.08 m 26 ft 6 in
2 PowerJet SaM146 turbofans engines 1x Pratt & Whitney J52-P-6A Jet
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 8,500 pound-force
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 8,500 pound-force
49,450 kg 109,000 lb MTOW 11,113 kg 24,500 lb
4,578 km 2,470 nm range 3,222 km 1,739 nm
515 mph 830 km/h cruise speed 586 kts 364 mph
98 (up to 108) passengers capacity Up to 9,155 pounds of weapons on 5 hardpoints
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.