McDonnell Douglas F-4 Phantom II vs. N. American T-28 Trojan

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McDonnell Douglas F-4 Phantom II versus N. American T-28 Trojan
19.2 m 63 ft 0 in length 10.06 m 33 ft 0 in
5.03 m 16 ft 6 in height 3.86 m 12 ft 8 in
11.72 m 38 ft 5 in wingspan 12.22 m 40 ft 1 in
Two General Electric J79s engines 1 x Wright R-1820-86 Cyclone radial engine
17,900 lbs thrust per engine Approximately 1,425 hp
35,800 lbs total thrust Approximately 1,425 hp
27,965 kg 61,700 lb MTOW 8,500 lb 3,856 kg
3,031 km 1,636 nm range 1,705 km 921 nm
Mach 2.2 2,717 km/h cruise speed 210 mph 338 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.