Cessna O-2 Skymaster vs. McDonnell Douglas F-4 Phantom II

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Cessna O-2 Skymaster versus McDonnell Douglas F-4 Phantom II
8.9 m 29 ft 2 in length 19.2 m 63 ft 0 in
2.87 m 9 ft 5 in height 5.03 m 16 ft 6 in
11.58 m 38 ft wingspan 11.72 m 38 ft 5 in
Two 210-hp Continental IO-360s engines Two General Electric J79s
210 hp thrust per engine 17,900 lbs
420 hp total thrust 35,800 lbs
5,400 lb 2,449 kg MTOW 27,965 kg 61,700 lb
1,705 km 921 nm range 3,031 km 1,636 nm
144 mph 232 km/h cruise speed Mach 2.2 2,717 km/h
2 capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.