Douglas DC-8-61 vs. de Havilland Canada DHC-2 Beaver
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Douglas DC-8-61 |
versus |
de Havilland Canada DHC-2 Beaver |
57.0 m |
187 ft 0 in |
length |
13.56 m |
44 ft 6 in |
13.1 m |
43 ft |
height |
5 m |
16 ft 5 in |
45.24 m |
148 ft 5 in |
wingspan |
16.56 m |
54 ft 4 in |
4x P&W JT3D-3B Turbofan |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
18,000 pound-force |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
72,000 pound-force |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
147,400 kg |
325,000 lb |
MTOW |
24,200 lb |
10,977 kg |
3,200 nm |
5,926 km |
range |
2,535 km |
1,369 nm |
483 knots |
282 mph |
cruise speed |
228 mph |
367 km/h |
180 to 220 passengers in a mixed-class seating |
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.