Avro Shackleton vs. Northrop T-38 Talon

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Avro Shackleton versus Northrop T-38 Talon
26.6 m 87 ft 4 in length 14.1 m 46 ft 4 in
6.22 m 20 ft 5 in height 3.9 m 12 ft 10 in
36.58 m 120 ft wingspan 7.7 m 25 ft 3 in
4 x Rolls-Royce Griffon 57 engines Two General Electric J85-GE-5A turbojet engines
1,960 horsepower thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
7,840 horsepower total thrust 4,100 pounds dry thrust; 5,800 with afterburners
39,009 kg 86,000 lb MTOW 12,093 lb 5,485 kg
3,621 km 1,955 nm range 1,759 km 950 nm
262 kts 163 mph cruise speed 745 kts 1,380 km/h
10,000lb of bombs, torpedoes or mines 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.