Boeing 777-9 vs. Northrop T-38 Talon
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Boeing 777-9 |
versus |
Northrop T-38 Talon |
76.72 m |
251 ft 9 in |
length |
14.1 m |
46 ft 4 in |
19.65 m |
64 ft 6 in |
height |
3.9 m |
12 ft 10 in |
71.75 m |
235 ft 5 in |
wingspan |
7.7 m |
25 ft 3 in |
GE9X |
engines |
Two General Electric J85-GE-5A turbojet engines |
105,000 lbf |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
210,000 lbf |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
351,550 kg |
775,000 lb |
MTOW |
12,093 lb |
5,485 kg |
13,500 km |
7,285 nmi |
range |
1,759 km |
950 nm |
590 mph |
950 km/h |
cruise speed |
745 kts |
1,380 km/h |
426 (Typical 2-class) |
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.