Sukhoi SSJ 100 95LR vs. de Havilland Canada DHC-2 Beaver
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Sukhoi SSJ 100 95LR |
versus |
de Havilland Canada DHC-2 Beaver |
29.94 m |
98 ft 2 in |
length |
13.56 m |
44 ft 6 in |
10.28 m |
33 ft 8 in |
height |
5 m |
16 ft 5 in |
27.8 m |
91 ft 2 in |
wingspan |
16.56 m |
54 ft 4 in |
2 PowerJet SaM146 turbofans |
engines |
2 x Armstrong Siddeley Double Mamba turboprop 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 3,100 hp (2,312 kW) each |
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 6,200 hp (4,624 kW) total |
49,450 kg |
109,000 lb |
MTOW |
24,200 lb |
10,977 kg |
4,578 km |
2,470 nm |
range |
2,535 km |
1,369 nm |
515 mph |
830 km/h |
cruise speed |
228 mph |
367 km/h |
98 (up to 108) passengers |
capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.