Douglas DC-8-61 vs. Lockheed U-2
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Douglas DC-8-61 |
versus |
Lockheed U-2 |
57.0 m |
187 ft 0 in |
length |
19.2 m |
63 ft 0 in |
13.1 m |
43 ft |
height |
4.8 m |
15 ft 9 in |
45.24 m |
148 ft 5 in |
wingspan |
32 m |
105 ft |
4x P&W JT3D-3B Turbofan |
engines |
1 × General Electric F118-101 |
18,000 pound-force |
thrust per engine |
17,000 lbf (76 kN) |
72,000 pound-force |
total thrust |
17,000 lbf (76 kN) |
147,400 kg |
325,000 lb |
MTOW |
18,144 kg |
40,000 lb |
3,200 nm |
5,926 km |
range |
6,090 nm |
11,278 km |
483 knots |
282 mph |
cruise speed |
475 mph |
764 km/h |
180 to 220 passengers in a mixed-class seating |
capacity |
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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.