McDonnell Douglas F-4 Phantom II vs. North American BT-9

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McDonnell Douglas F-4 Phantom II versus North American BT-9
19.2 m 63 ft 0 in length 8.79 m 28 ft 10 in
5.03 m 16 ft 6 in height 2.82 m 9 ft 3 in
11.72 m 38 ft 5 in wingspan 10.97 m 36 ft
Two General Electric J79s engines 1 x Wright R-975-3 radial engine
17,900 lbs thrust per engine Approximately 440 hp
35,800 lbs total thrust Approximately 440 hp
27,965 kg 61,700 lb MTOW 4,300 lb 1,950 kg
3,031 km 1,636 nm range 917 km 495 nm
Mach 2.2 2,717 km/h cruise speed 150 mph 241 km/h
Up to 16,000 lbs of externally carried ordnance capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.