Bombardier CRJ900 vs. McDonnell Douglas F-4 Phantom II

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Bombardier CRJ900 versus McDonnell Douglas F-4 Phantom II
36.2 m 118 ft 11 in length 19.2 m 63 ft 0 in
7.5 m 24 ft 7 in height 5.03 m 16 ft 6 in
24.9 m 81 ft 8 in wingspan 11.72 m 38 ft 5 in
2 Turbofans (fuselage mounted) engines Two General Electric J79s
13,360 pounds force thrust per engine 17,900 lbs
26,720 pounds force total thrust 35,800 lbs
38,330 kg 84,500 lb MTOW 27,965 kg 61,700 lb
2,871 km 1,550 nm range 3,031 km 1,636 nm
515 mph 829 km/h cruise speed Mach 2.2 2,717 km/h
Up to 90 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.