McDonnell Douglas F-4 Phantom II vs. North American B-25 Mitchell

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McDonnell Douglas F-4 Phantom II versus North American B-25 Mitchell
19.2 m 63 ft 0 in length 16.15 m 53 ft 0 in
5.03 m 16 ft 6 in height 5 m 16 ft 4 in
11.72 m 38 ft 5 in wingspan 20.58 m 67 ft 6 in
Two General Electric J79s engines 2 x Wright R-2600-92 Twin Cyclone
17,900 lbs thrust per engine 1,700 horsepower
35,800 lbs total thrust 3,400 horsepower
27,965 kg 61,700 lb MTOW 7,484 kg 16,500 lb
3,031 km 1,636 nm range 1,350 mi 1,175 nm
Mach 2.2 2,717 km/h cruise speed 233 MPH 375 km/h
Up to 16,000 lbs of externally carried ordnance capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.