Lockheed T-33 Shooting Star vs. Northrop T-38 Talon
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Lockheed T-33 Shooting Star |
versus |
Northrop T-38 Talon |
11.51 m |
37 ft 9 in |
length |
14.1 m |
46 ft 4 in |
3.56 m |
11 ft 8 in |
height |
3.9 m |
12 ft 10 in |
11.9 m |
39 ft 1 in |
wingspan |
7.7 m |
25 ft 3 in |
1 (Allison J33-A-5) |
engines |
Two General Electric J85-GE-5A turbojet engines |
24.0 kN |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
24.0 kN |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
5,900 kg |
13,000 lb |
MTOW |
12,093 lb |
5,485 kg |
2,050 km |
1,107 nm |
range |
1,759 km |
950 nm |
965 km/h |
600 mph |
cruise speed |
745 kts |
1,380 km/h |
907 kg of bombs or rockets |
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.