Boeing 787-9 vs. Lockheed U-2
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Boeing 787-9 |
versus |
Lockheed U-2 |
63.0 m |
206 ft 9 in |
length |
19.2 m |
63 ft 0 in |
17 m |
55 ft 9 in |
height |
4.8 m |
15 ft 9 in |
60 m |
196 ft 1 |
wingspan |
32 m |
105 ft |
GEnx-1B / Trent 1000 |
engines |
1 × General Electric F118-101 |
76,100 pounds |
thrust per engine |
17,000 lbf (76 kN) |
152,200 pounds |
total thrust |
17,000 lbf (76 kN) |
254,000 kg |
560,000 lb |
MTOW |
18,144 kg |
40,000 lb |
14,140 km |
7,635 nmi |
range |
6,090 nm |
11,278 km |
652 mph |
1,050 kph |
cruise speed |
475 mph |
764 km/h |
290 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.