McDonnell Douglas F-4 Phantom II vs. Cirrus Vision SF50

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McDonnell Douglas F-4 Phantom II versus Cirrus Vision SF50
19.2 m 63 ft 0 in length 9.36 m 30 ft 9 in
5.03 m 16 ft 6 in height 3.32 m 10 ft 11 in
11.72 m 38 ft 5 in wingspan 11.79 m 38 ft 8 in
Two General Electric J79s engines 1 x Williams FJ33
17,900 lbs thrust per engine 1800 lbs
35,800 lbs total thrust 1800 lbs
27,965 kg 61,700 lb MTOW 6,000 lb 2,722 kg
3,031 km 1,636 nm range 1240 nm 2,296 km
Mach 2.2 2,717 km/h cruise speed 300 kts 186 mph
Up to 16,000 lbs of externally carried ordnance capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.