Lockheed Martin F-22 Raptor vs. Northrop T-38 Talon
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Lockheed Martin F-22 Raptor |
versus |
Northrop T-38 Talon |
18.9 m |
62 ft 1 in |
length |
14.1 m |
46 ft 4 in |
5.1 m |
16 ft 9 in |
height |
3.9 m |
12 ft 10 in |
13.6 m |
44 ft 7 in |
wingspan |
7.7 m |
25 ft 3 in |
Two Pratt & Whitney F119-PW-100 turbofan engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
35,000-pound class |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
70,000-pound class |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
38,000 kg |
83,500 lb |
MTOW |
12,093 lb |
5,485 kg |
1,850 mi |
1,611 nm |
range |
1,759 km |
950 nm |
Mach 1.6 |
1976 km/h |
cruise speed |
745 kts |
1,380 km/h |
|
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.