Bombardier CS100 vs. Lockheed Martin C-130J Super Hercules
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Bombardier CS100 |
versus |
Lockheed Martin C-130J Super Hercules |
35.00 m |
114 ft 10 in |
length |
34.37 m |
112 ft 9 in |
11.5 m |
37 ft 9 in |
height |
11.86 m |
38 ft 11 in |
35.1 m |
115 ft 2 in |
wingspan |
40.41 m |
132 ft 7 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
84.1 kN |
thrust per engine |
Approximately 4,700 hp per engine |
168.2 kN |
total thrust |
Approximately 18,800 hp total |
54,931 kg |
121,100 lb |
MTOW |
76,610 kg |
168,900 lb |
4,074 km |
2,200 nm |
range |
4,600 km |
2,485 nm |
871 km/h |
541 mph |
cruise speed |
660 km/h |
410 mph |
110 passengers |
capacity |
based on configuration |
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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.