McDonnell Douglas F-4 Phantom II vs. Lockheed C-69 Constellation

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McDonnell Douglas F-4 Phantom II versus Lockheed C-69 Constellation
19.2 m 63 ft 0 in length 29.72 m 97 ft 6 in
5.03 m 16 ft 6 in height 6.02 m 19 ft 9 in
11.72 m 38 ft 5 in wingspan 37.49 m 123 ft
Two General Electric J79s engines 4 x Wright R-3350 Duplex-Cyclone radial engines
17,900 lbs thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
35,800 lbs total thrust 8,800 to 14,800 horsepower
27,965 kg 61,700 lb MTOW 44,453 kg 98,000 lb
3,031 km 1,636 nm range 5,200 km 2,808 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 109 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.