Boeing 777-200LR Worldliner vs. Northrop T-38 Talon
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Boeing 777-200LR Worldliner |
versus |
Northrop T-38 Talon |
63.7 m |
209 ft 1 in |
length |
14.1 m |
46 ft 4 in |
18.6 m |
61 ft |
height |
3.9 m |
12 ft 10 in |
64.8 m |
212 ft 7 in |
wingspan |
7.7 m |
25 ft 3 in |
2 x GE90-115B |
engines |
Two General Electric J85-GE-5A turbojet engines |
115,300 lbf |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
230,600 lbf |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
347,500 kg |
766,100 lb |
MTOW |
12,093 lb |
5,485 kg |
15,843 km |
8,555 nmi |
range |
1,759 km |
950 nm |
950 km/h |
590 mph |
cruise speed |
745 kts |
1,380 km/h |
317 (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.