Bombardier CRJ700 vs. Lockheed U-2
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Bombardier CRJ700 |
versus |
Lockheed U-2 |
32.51 m |
106 ft 8 in |
length |
19.2 m |
63 ft 0 in |
7.6 m |
24 ft 11 in |
height |
4.8 m |
15 ft 9 in |
23.24 m |
76 ft 3 in |
wingspan |
32 m |
105 ft |
2 x General Electric CF34-8C5B1 turbofans |
engines |
1 × General Electric F118-101 |
13,790 pounds (61.3 kN) |
thrust per engine |
17,000 lbf (76 kN) |
27,580 pounds (122.6 kN) |
total thrust |
17,000 lbf (76 kN) |
33,113 kg |
73,000 lb |
MTOW |
18,144 kg |
40,000 lb |
2,655 km |
1,434 nm |
range |
6,090 nm |
11,278 km |
514 mph |
828 km/h |
cruise speed |
475 mph |
764 km/h |
Up to 78 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.