Airbus A319 vs. Northrop T-38 Talon
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Airbus A319 |
versus |
Northrop T-38 Talon |
33.84 m |
111 ft 0 in |
length |
14.1 m |
46 ft 4 in |
11.76 m |
38 ft 7 in |
height |
3.9 m |
12 ft 10 in |
35.8 m |
117 ft 5 in |
wingspan |
7.7 m |
25 ft 3 in |
2 (International Aero Engines V2524-A5) |
engines |
Two General Electric J85-GE-5A turbojet engines |
27,000 lb |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
54,000 lb |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
75,500 kg |
166,400 lb |
MTOW |
12,093 lb |
5,485 kg |
3,700 nmi |
6,852 km |
range |
1,759 km |
950 nm |
829 km/h |
515 mph |
cruise speed |
745 kts |
1,380 km/h |
124 to 156 passengers |
capacity |
Two (student and instructor) |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.