Bombardier CS100 vs. McDonnell Douglas F-4 Phantom II
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Bombardier CS100 |
versus |
McDonnell Douglas F-4 Phantom II |
35.00 m |
114 ft 10 in |
length |
19.2 m |
63 ft 0 in |
11.5 m |
37 ft 9 in |
height |
5.03 m |
16 ft 6 in |
35.1 m |
115 ft 2 in |
wingspan |
11.72 m |
38 ft 5 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
Two General Electric J79s |
84.1 kN |
thrust per engine |
17,900 lbs |
168.2 kN |
total thrust |
35,800 lbs |
54,931 kg |
121,100 lb |
MTOW |
27,965 kg |
61,700 lb |
4,074 km |
2,200 nm |
range |
3,031 km |
1,636 nm |
871 km/h |
541 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
110 passengers |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.