McDonnell Douglas F-4 Phantom II vs. North American T-6 Texan

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McDonnell Douglas F-4 Phantom II versus North American T-6 Texan
19.2 m 63 ft 0 in length 9.0 m 29 ft 6 in
5.03 m 16 ft 6 in height 3.56 m 11 ft 8 in
11.72 m 38 ft 5 in wingspan 12.8 m 42 ft
Two General Electric J79s engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
17,900 lbs thrust per engine Approximately 600 hp
35,800 lbs total thrust Approximately 600 hp
27,965 kg 61,700 lb MTOW 5,617 lb 2,548 kg
3,031 km 1,636 nm range 1,175 km 634 nm
Mach 2.2 2,717 km/h cruise speed 145 mph 233 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.