Avro 652 Anson vs. Northrop T-38 Talon

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Avro 652 Anson versus Northrop T-38 Talon
12.88 m 42 ft 3 in length 14.1 m 46 ft 4 in
2.9 m 9 ft 6 in height 3.9 m 12 ft 10 in
17.22 m 56 ft 6 in wingspan 7.7 m 25 ft 3 in
2 × Armstrong Siddeley Cheetah VI engines Two General Electric J85-GE-5A turbojet engines
290 hp (220 kW) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
580 hp (440 kW) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
7,500 lb 3,402 kg MTOW 12,093 lb 5,485 kg
1,267 km 684 nm range 1,759 km 950 nm
165 mph 266 km/h cruise speed 745 kts 1,380 km/h
4 passengers capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.