Avro 652 Anson vs. Lockheed Martin F-35 Lightning II

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Avro 652 Anson versus Lockheed Martin F-35 Lightning II
12.88 m 42 ft 3 in length 15.67 m 51 ft 4 in
2.9 m 9 ft 6 in height 4.33 m 14 ft 2 in
17.22 m 56 ft 6 in wingspan 10.7 m 35 ft 1 in
2 × Armstrong Siddeley Cheetah VI engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
290 hp (220 kW) thrust per engine 40,000 lb
580 hp (440 kW) total thrust 40,000 lb
7,500 lb 3,402 kg MTOW 31,800 kg 70,000 lb
1,267 km 684 nm range 1,380 mi 1,200 nm
165 mph 266 km/h cruise speed 520 kt 302 mph
4 passengers capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.