McDonnell Douglas F-4 Phantom II vs. Aero Commander 500S

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McDonnell Douglas F-4 Phantom II versus Aero Commander 500S
19.2 m 63 ft 0 in length 10.46 m 34 ft 4 in
5.03 m 16 ft 6 in height 3.63 m 11 ft 11 in
11.72 m 38 ft 5 in wingspan 13.52 m 44 ft 4 in
Two General Electric J79s engines 2 x Lycoming IO-540
17,900 lbs thrust per engine 380 lbs
35,800 lbs total thrust 760 lbs
27,965 kg 61,700 lb MTOW 11,500 lb 5,216 kg
3,031 km 1,636 nm range 1,350 nm 2,500 km
Mach 2.2 2,717 km/h cruise speed 230 kts 143 mph
Up to 16,000 lbs of externally carried ordnance capacity Up to 4 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.