Tupolev TU-155 vs. de Havilland Canada DHC-2 Beaver
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| Tupolev TU-155 |
versus |
de Havilland Canada DHC-2 Beaver |
| 47.63 m |
156 ft 3 in |
length |
13.56 m |
44 ft 6 in |
| 16.4 m |
53 ft 10 in |
height |
5 m |
16 ft 5 in |
| 64.9 m |
212 ft 11 in |
wingspan |
16.56 m |
54 ft 4 in |
| 4 × Kuznetsov NK-321 turbofans |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
| 304.5 kN (68,500 lbf) |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
| 1,218 kN (274,000 lbf) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
| 640,000 kg |
1,411,000 lb |
MTOW |
24,200 lb |
10,977 kg |
| 7,000 km |
3,780 nm |
range |
2,535 km |
1,369 nm |
| 850 km/h |
528 mph |
cruise speed |
228 mph |
367 km/h |
| 350 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.
