de Havilland Venom vs. McDonnell Douglas F-4 Phantom II

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de Havilland Venom versus McDonnell Douglas F-4 Phantom II
6.71 m 22 ft 0 in length 19.2 m 63 ft 0 in
1.88 m 6 ft 2 in height 5.03 m 16 ft 6 in
12.7 m 41 ft 8 in wingspan 11.72 m 38 ft 5 in
1 (de Havilland Ghost 105) engines Two General Electric J79s
23.6 kN thrust per engine 17,900 lbs
23.6 kN total thrust 35,800 lbs
6,945 kg 15,300 lb MTOW 27,965 kg 61,700 lb
1,730 km 935 nm range 3,031 km 1,636 nm
1030 km/h 640 mph cruise speed Mach 2.2 2,717 km/h
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.