Bombardier CS100 vs. Lockheed U-2
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Bombardier CS100 |
versus |
Lockheed U-2 |
35.00 m |
114 ft 10 in |
length |
19.2 m |
63 ft 0 in |
11.5 m |
37 ft 9 in |
height |
4.8 m |
15 ft 9 in |
35.1 m |
115 ft 2 in |
wingspan |
32 m |
105 ft |
2 x Pratt & Whitney PurePower PW1500G |
engines |
1 × General Electric F118-101 |
84.1 kN |
thrust per engine |
17,000 lbf (76 kN) |
168.2 kN |
total thrust |
17,000 lbf (76 kN) |
54,931 kg |
121,100 lb |
MTOW |
18,144 kg |
40,000 lb |
4,074 km |
2,200 nm |
range |
6,090 nm |
11,278 km |
871 km/h |
541 mph |
cruise speed |
475 mph |
764 km/h |
110 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.