Northrop T-38 Talon vs. Airbus A300-600F

versus
... or view the full comparison list here.
Northrop T-38 Talon versus Airbus A300-600F
14.1 m 46 ft 4 in length 54.08 m 177 ft 5 in
3.9 m 12 ft 10 in height 17.05 m 55 ft 11 in
7.7 m 25 ft 3 in wingspan 44.84 m 147 ft 1 in
Two General Electric J85-GE-5A turbojet engines engines 2 x General Electric CF6-80C2A5 turbofan engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 59,000 lbf per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 118,000 lbf total
12,093 lb 5,485 kg MTOW 170,000 kg 374,786 lb
1,759 km 950 nm range 4,830 km 2,608 nm
745 kts 1,380 km/h cruise speed 860 km/h 534 mph
Two (student and instructor) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.