Airbus A318 vs. Northrop T-38 Talon
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Airbus A318 |
versus |
Northrop T-38 Talon |
31.44 m |
103 ft 2 in |
length |
14.1 m |
46 ft 4 in |
12.56 m |
41 ft 3 in |
height |
3.9 m |
12 ft 10 in |
34.1 m |
111 ft 11 in |
wingspan |
7.7 m |
25 ft 3 in |
2x CFM56-5B or 2x PW6000 |
engines |
Two General Electric J85-GE-5A turbojet engines |
23,300 lb |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
46,600 lb |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
59,000 kg |
130,000 lb |
MTOW |
12,093 lb |
5,485 kg |
5,750 km |
3,106 nm |
range |
1,759 km |
950 nm |
963km/h |
598mph |
cruise speed |
745 kts |
1,380 km/h |
107 to 132 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.