McDonnell Douglas F-4 Phantom II vs. Douglas DC-6

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McDonnell Douglas F-4 Phantom II versus Douglas DC-6
19.2 m 63 ft 0 in length 32.18 m 105 ft 7 in
5.03 m 16 ft 6 in height 8.94 m 29 ft 4 in
11.72 m 38 ft 5 in wingspan 35.81 m 117 ft 6 in
Two General Electric J79s engines 4 x Pratt & Whitney R-2800-CB17 radial engines
17,900 lbs thrust per engine Approximately 2,500 hp per engine
35,800 lbs total thrust Approximately 10,000 hp total
27,965 kg 61,700 lb MTOW 52,200 kg 115,100 lb
3,031 km 1,636 nm range 5,800 km 3,133 nm
Mach 2.2 2,717 km/h cruise speed 507 km/h 315 mph
Up to 16,000 lbs of externally carried ordnance capacity Up to 102 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.