Boeing 747-8I vs. Northrop T-38 Talon
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Boeing 747-8I |
versus |
Northrop T-38 Talon |
76.25 m |
250 ft 2 in |
length |
14.1 m |
46 ft 4 in |
19.35 m |
63 ft 6 in |
height |
3.9 m |
12 ft 10 in |
68.45 m |
224 ft 7 in |
wingspan |
7.7 m |
25 ft 3 in |
4x General Electric GEnx 2B67 Turbofan |
engines |
Two General Electric J85-GE-5A turbojet engines |
66,500 pounds |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
266,000 pounds |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
443,613 kg |
977,500 lb |
MTOW |
12,093 lb |
5,485 kg |
8,000 nm |
14,816 km |
range |
1,759 km |
950 nm |
Mach 0.86 |
1,062 km/h |
cruise speed |
745 kts |
1,380 km/h |
467 passengers (three-class configuration) |
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.