Lockheed F-104 Starfighter vs. Northrop T-38 Talon

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Lockheed F-104 Starfighter versus Northrop T-38 Talon
16.69 m 54 ft 9 in length 14.1 m 46 ft 4 in
4.11 m 13 ft 6 in height 3.9 m 12 ft 10 in
6.68 m 21 ft 11 in wingspan 7.7 m 25 ft 3 in
1 Turbojet Engine engines Two General Electric J85-GE-5A turbojet engines
46.7 / 71.2 kN (dry/with Afterburner) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
46.7 / 71.2 kN (dry/with Afterburner) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
13,500 kg 29,800 lb MTOW 12,093 lb 5,485 kg
1,200 km 648 nm range 1,759 km 950 nm
510 mph 821 km/h cruise speed 745 kts 1,380 km/h
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.