Sukhoi SSJ 100 95LR vs. Lockheed P-2 Neptune

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Sukhoi SSJ 100 95LR versus Lockheed P-2 Neptune
29.94 m 98 ft 2 in length 30.17 m 99 ft 0 in
10.28 m 33 ft 8 in height 10.15 m 33 ft 4 in
27.8 m 91 ft 2 in wingspan 33.53 m 110 ft
2 PowerJet SaM146 turbofans engines 2 x Wright R-3350 radial engines
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 Approximately 3,700 hp
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 Approximately 7,400 hp
49,450 kg 109,000 lb MTOW 27,216 kg 60,000 lb
4,578 km 2,470 nm range 7,885 km 4,259 nm
515 mph 830 km/h cruise speed 300 mph 483 km/h
98 (up to 108) passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.