Avro Vulcan vs. McDonnell Douglas F-4 Phantom II

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Avro Vulcan versus McDonnell Douglas F-4 Phantom II
30.46 m 99 ft 11 in length 19.2 m 63 ft 0 in
8.28 m 27 ft 2 in height 5.03 m 16 ft 6 in
33.53 m 110 ft wingspan 11.72 m 38 ft 5 in
4 Bristol Olympus engines Two General Electric J79s
20,000 lbs thrust per engine 17,900 lbs
80,000 lbs total thrust 35,800 lbs
35,000 kg 77,200 lb MTOW 27,965 kg 61,700 lb
2,592 nm 4,798 km range 3,031 km 1,636 nm
1,010 km/h 627 mph cruise speed Mach 2.2 2,717 km/h
10,000 kg payload 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.