McDonnell Douglas F-4 Phantom II vs. Cessna 152

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McDonnell Douglas F-4 Phantom II versus Cessna 152
19.2 m 63 ft 0 in length 7.34 m 24 ft 1 in
5.03 m 16 ft 6 in height 2.59 m 8 ft 6 in
11.72 m 38 ft 5 in wingspan 10.16 m 33 ft 4 in
Two General Electric J79s engines 1 x Lycoming O-235-L2C flat-4 piston engine
17,900 lbs thrust per engine 115 horsepower (86 kW)
35,800 lbs total thrust 115 horsepower (86 kW)
27,965 kg 61,700 lb MTOW 757 kg 1,669 lb
3,031 km 1,636 nm range 610 km 329 nm
Mach 2.2 2,717 km/h cruise speed 185 km/h 115 mph
Up to 16,000 lbs of externally carried ordnance capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.