Lockheed L-1011 TriStar 500 vs. Northrop T-38 Talon
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Lockheed L-1011 TriStar 500 |
versus |
Northrop T-38 Talon |
50.05 m |
164 ft 3 in |
length |
14.1 m |
46 ft 4 in |
16.87 m |
55 ft 4 in |
height |
3.9 m |
12 ft 10 in |
50.09 m |
164 ft 4 in |
wingspan |
7.7 m |
25 ft 3 in |
3 Rolls-Royce RB211 engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
42,000 lbf |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
126,000 lbf (3 engines x 42,000 lbf per engine) |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
231,330 kg |
510,000 lb |
MTOW |
12,093 lb |
5,485 kg |
11,260 km |
6,100 nm |
range |
1,759 km |
950 nm |
525 knots |
972 km/h |
cruise speed |
745 kts |
1,380 km/h |
Max. 315 passengers (typical 253) |
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.