Avro 652 Anson vs. McDonnell Douglas F-4 Phantom II

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Avro 652 Anson versus McDonnell Douglas F-4 Phantom II
12.88 m 42 ft 3 in length 19.2 m 63 ft 0 in
2.9 m 9 ft 6 in height 5.03 m 16 ft 6 in
17.22 m 56 ft 6 in wingspan 11.72 m 38 ft 5 in
2 × Armstrong Siddeley Cheetah VI engines Two General Electric J79s
290 hp (220 kW) thrust per engine 17,900 lbs
580 hp (440 kW) total thrust 35,800 lbs
7,500 lb 3,402 kg MTOW 27,965 kg 61,700 lb
1,267 km 684 nm range 3,031 km 1,636 nm
165 mph 266 km/h cruise speed Mach 2.2 2,717 km/h
4 passengers 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.