Douglas DC-8-61 vs. McDonnell Douglas F-4 Phantom II

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Douglas DC-8-61 versus McDonnell Douglas F-4 Phantom II
57.0 m 187 ft 0 in length 19.2 m 63 ft 0 in
13.1 m 43 ft height 5.03 m 16 ft 6 in
45.24 m 148 ft 5 in wingspan 11.72 m 38 ft 5 in
4x P&W JT3D-3B Turbofan engines Two General Electric J79s
18,000 pound-force thrust per engine 17,900 lbs
72,000 pound-force total thrust 35,800 lbs
147,400 kg 325,000 lb MTOW 27,965 kg 61,700 lb
3,200 nm 5,926 km range 3,031 km 1,636 nm
483 knots 282 mph cruise speed Mach 2.2 2,717 km/h
180 to 220 passengers in a mixed-class seating 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.