McDonnell-Douglas DC-10-30 vs. Lockheed U-2
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McDonnell-Douglas DC-10-30 |
versus |
Lockheed U-2 |
55.35 m |
181 ft 8 in |
length |
19.2 m |
63 ft 0 in |
17.8 m |
58 ft 5 in |
height |
4.8 m |
15 ft 9 in |
50.39 m |
165 ft 4 in |
wingspan |
32 m |
105 ft |
3x GE CF6-50C Turbofan |
engines |
1 × General Electric F118-101 |
54,000 lbf |
thrust per engine |
17,000 lbf (76 kN) |
162,000 lbf |
total thrust |
17,000 lbf (76 kN) |
251,744 kg |
555,000 lb |
MTOW |
18,144 kg |
40,000 lb |
9,630 km |
5,200 nm |
range |
6,090 nm |
11,278 km |
507 knots |
939 km/h |
cruise speed |
475 mph |
764 km/h |
Up to 380 passengers |
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.