Avro Shackleton vs. McDonnell Douglas F-4 Phantom II

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Avro Shackleton versus McDonnell Douglas F-4 Phantom II
26.6 m 87 ft 4 in length 19.2 m 63 ft 0 in
6.22 m 20 ft 5 in height 5.03 m 16 ft 6 in
36.58 m 120 ft wingspan 11.72 m 38 ft 5 in
4 x Rolls-Royce Griffon 57 engines Two General Electric J79s
1,960 horsepower thrust per engine 17,900 lbs
7,840 horsepower total thrust 35,800 lbs
39,009 kg 86,000 lb MTOW 27,965 kg 61,700 lb
3,621 km 1,955 nm range 3,031 km 1,636 nm
262 kts 163 mph cruise speed Mach 2.2 2,717 km/h
10,000lb of bombs, torpedoes or mines 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.