Bombardier CRJ1000 vs. McDonnell Douglas F-4 Phantom II

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Bombardier CRJ1000 versus McDonnell Douglas F-4 Phantom II
39.1 m 128 ft 5 in length 19.2 m 63 ft 0 in
7.5 m 24 ft 7 in height 5.03 m 16 ft 6 in
26.2 m 86 ft wingspan 11.72 m 38 ft 5 in
2 GE CF34-8C5A1 turbofans engines Two General Electric J79s
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 17,900 lbs
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 35,800 lbs
41,640 kg 91,800 lb MTOW 27,965 kg 61,700 lb
3,004 km 1,623 nm range 3,031 km 1,636 nm
515 mph 829 km/h cruise speed Mach 2.2 2,717 km/h
100 (common) 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.