Bombardier CS100 vs. Lockheed P-2 Neptune
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Bombardier CS100 |
versus |
Lockheed P-2 Neptune |
35.00 m |
114 ft 10 in |
length |
30.17 m |
99 ft 0 in |
11.5 m |
37 ft 9 in |
height |
10.15 m |
33 ft 4 in |
35.1 m |
115 ft 2 in |
wingspan |
33.53 m |
110 ft |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Wright R-3350 radial engines |
84.1 kN |
thrust per engine |
Approximately 3,700 hp |
168.2 kN |
total thrust |
Approximately 7,400 hp |
54,931 kg |
121,100 lb |
MTOW |
27,216 kg |
60,000 lb |
4,074 km |
2,200 nm |
range |
7,885 km |
4,259 nm |
871 km/h |
541 mph |
cruise speed |
300 mph |
483 km/h |
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.