Boeing 717-200HGW vs. Northrop T-38 Talon

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Boeing 717-200HGW versus Northrop T-38 Talon
37.80 m 123 ft 11 in length 14.1 m 46 ft 4 in
8.87 m 29 ft 1 in height 3.9 m 12 ft 10 in
28.44 m 93 ft 4 in wingspan 7.7 m 25 ft 3 in
2 Rolls-Royce BR715 engines Two General Electric J85-GE-5A turbojet engines
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
54,885 kg 121,000 lb MTOW 12,093 lb 5,485 kg
2,060 nm 3,814 km range 1,759 km 950 nm
811 km/h 504 mph cruise speed 745 kts 1,380 km/h
106 passengers in a 2 class configuration 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.