Douglas DC-8-61 vs. Lockheed P-2 Neptune
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Douglas DC-8-61 |
versus |
Lockheed P-2 Neptune |
57.0 m |
187 ft 0 in |
length |
30.17 m |
99 ft 0 in |
13.1 m |
43 ft |
height |
10.15 m |
33 ft 4 in |
45.24 m |
148 ft 5 in |
wingspan |
33.53 m |
110 ft |
4x P&W JT3D-3B Turbofan |
engines |
2 x Wright R-3350 radial engines |
18,000 pound-force |
thrust per engine |
Approximately 3,700 hp |
72,000 pound-force |
total thrust |
Approximately 7,400 hp |
147,400 kg |
325,000 lb |
MTOW |
27,216 kg |
60,000 lb |
3,200 nm |
5,926 km |
range |
7,885 km |
4,259 nm |
483 knots |
282 mph |
cruise speed |
300 mph |
483 km/h |
180 to 220 passengers in a mixed-class seating |
capacity |
based on configuration |
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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.