de Havilland Canada DHC-2 Beaver vs. Douglas DC-8
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de Havilland Canada DHC-2 Beaver |
versus |
Douglas DC-8 |
13.56 m |
44 ft 6 in |
length |
57.10 m |
187 ft 4 in |
5 m |
16 ft 5 in |
height |
16.84 m |
55 ft 3 in |
16.56 m |
54 ft 4 in |
wingspan |
45.24 m |
148 ft 5 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
4 x Pratt & Whitney JT3D turbofan engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 17,000 lbf per engine |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 68,000 lbf total |
24,200 lb |
10,977 kg |
MTOW |
158,760 kg |
350,000 lb |
2,535 km |
1,369 nm |
range |
11,918 km |
6,437 nm |
228 mph |
367 km/h |
cruise speed |
900 km/h |
559 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
Up to 259 passengers |
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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.