Bombardier CRJ700 vs. McDonnell Douglas F-4 Phantom II

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Bombardier CRJ700 versus McDonnell Douglas F-4 Phantom II
32.51 m 106 ft 8 in length 19.2 m 63 ft 0 in
7.6 m 24 ft 11 in height 5.03 m 16 ft 6 in
23.24 m 76 ft 3 in wingspan 11.72 m 38 ft 5 in
2 x General Electric CF34-8C5B1 turbofans engines Two General Electric J79s
13,790 pounds (61.3 kN) thrust per engine 17,900 lbs
27,580 pounds (122.6 kN) total thrust 35,800 lbs
33,113 kg 73,000 lb MTOW 27,965 kg 61,700 lb
2,655 km 1,434 nm range 3,031 km 1,636 nm
514 mph 828 km/h cruise speed Mach 2.2 2,717 km/h
Up to 78 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.