McDonnell Douglas F-4 Phantom II vs. Bell 412

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McDonnell Douglas F-4 Phantom II versus Bell 412
19.2 m 63 ft 0 in length 17,10 m 56 ft 1 in
5.03 m 16 ft 6 in height 3,48 m 11 ft 5 in
11.72 m 38 ft 5 in wingspan
Two General Electric J79s engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
17,900 lbs thrust per engine 1,800 hp
35,800 lbs total thrust 3,600 hp
27,965 kg 61,700 lb MTOW 5,400 kg 11,905 lb
3,031 km 1,636 nm range 659 km 356 nm
Mach 2.2 2,717 km/h cruise speed 259 km/h 161 mph
Up to 16,000 lbs of externally carried ordnance capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.