Lockheed P-38 Lightning vs. Northrop T-38 Talon
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Lockheed P-38 Lightning |
versus |
Northrop T-38 Talon |
11.53 m |
37 ft 10 in |
length |
14.1 m |
46 ft 4 in |
3.91 m |
12 ft 10 in |
height |
3.9 m |
12 ft 10 in |
15.85 m |
52 ft |
wingspan |
7.7 m |
25 ft 3 in |
Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
1,425 hp |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
2,850 hp |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
9,798 kg |
21,600 lb |
MTOW |
12,093 lb |
5,485 kg |
1,100 nm |
2,037 km |
range |
1,759 km |
950 nm |
239 knots |
139 mph |
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.