Bombardier CRJ900 vs. Lockheed U-2
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Bombardier CRJ900 |
versus |
Lockheed U-2 |
36.2 m |
118 ft 11 in |
length |
19.2 m |
63 ft 0 in |
7.5 m |
24 ft 7 in |
height |
4.8 m |
15 ft 9 in |
24.9 m |
81 ft 8 in |
wingspan |
32 m |
105 ft |
2 Turbofans (fuselage mounted) |
engines |
1 × General Electric F118-101 |
13,360 pounds force |
thrust per engine |
17,000 lbf (76 kN) |
26,720 pounds force |
total thrust |
17,000 lbf (76 kN) |
38,330 kg |
84,500 lb |
MTOW |
18,144 kg |
40,000 lb |
2,871 km |
1,550 nm |
range |
6,090 nm |
11,278 km |
515 mph |
829 km/h |
cruise speed |
475 mph |
764 km/h |
Up to 90 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.