McDonnell-Douglas DC-9-30 vs. Lockheed U-2
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McDonnell-Douglas DC-9-30 |
versus |
Lockheed U-2 |
36.36 m |
119 ft 3 in |
length |
19.2 m |
63 ft 0 in |
8.5 m |
27 ft 11 in |
height |
4.8 m |
15 ft 9 in |
28.44 m |
93 ft 4 in |
wingspan |
32 m |
105 ft |
2x Pratt & Whitney JT8D |
engines |
1 × General Electric F118-101 |
15,000 pound-force |
thrust per engine |
17,000 lbf (76 kN) |
30,000 pound-force (2 engines) |
total thrust |
17,000 lbf (76 kN) |
54,885 kg |
121,000 lb |
MTOW |
18,144 kg |
40,000 lb |
2,632 km |
1,422 nm |
range |
6,090 nm |
11,278 km |
898 km/h |
558 mph |
cruise speed |
475 mph |
764 km/h |
Up to 139 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.