Cessna A-37 Dragonfly vs. McDonnell Douglas F-4 Phantom II

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Cessna A-37 Dragonfly versus McDonnell Douglas F-4 Phantom II
8.617 m 28 ft 3 in length 19.2 m 63 ft 0 in
2.71 m 8 ft 11 in height 5.03 m 16 ft 6 in
10.94 m 35 ft 11 in wingspan 11.72 m 38 ft 5 in
2 x General Electric J85-GE-17A turbojets engines Two General Electric J79s
2,850 lbs thrust per engine 17,900 lbs
2 x 2,850 lbs = 5,700 lbs total thrust 35,800 lbs
6,350 kg 14,000 lb MTOW 27,965 kg 61,700 lb
460 nmi 852 km range 3,031 km 1,636 nm
489 mph 787 km/h cruise speed Mach 2.2 2,717 km/h
3,000 pounds of bombs, rockets and missiles capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.