Bombardier CS300 vs. McDonnell Douglas F-4 Phantom II

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Bombardier CS300 versus McDonnell Douglas F-4 Phantom II
38.0 m 124 ft 7 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
2x Pratt & Whitney PurePower PW1000G engines Two General Electric J79s
93.4 kN thrust per engine 17,900 lbs
186.8 kN total thrust 35,800 lbs
67,585 kg 149,000 lb MTOW 27,965 kg 61,700 lb
5,463 km 2,952 nm range 3,031 km 1,636 nm
871 km/h 541 mph cruise speed Mach 2.2 2,717 km/h
130 to 145 passengers capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.