Airbus A330-900neo vs. Northrop T-38 Talon
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Airbus A330-900neo |
versus |
Northrop T-38 Talon |
63.66 m |
208 ft 10 in |
length |
14.1 m |
46 ft 4 in |
16.79 m |
55 ft 1 in |
height |
3.9 m |
12 ft 10 in |
64 m |
210 ft |
wingspan |
7.7 m |
25 ft 3 in |
2x Rolls-Royce Trent 7000-72 Turbofan |
engines |
Two General Electric J85-GE-5A turbojet engines |
72,834 pound-force |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
144,000 lbf |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
251,000 kg |
553,400 lb |
MTOW |
12,093 lb |
5,485 kg |
7,200 nm |
13,334 km |
range |
1,759 km |
950 nm |
496 knots |
919 km/h |
cruise speed |
745 kts |
1,380 km/h |
260-300 |
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.