McDonnell-Douglas DC-10-30 vs. Northrop T-38 Talon
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McDonnell-Douglas DC-10-30 |
versus |
Northrop T-38 Talon |
55.35 m |
181 ft 8 in |
length |
14.1 m |
46 ft 4 in |
17.8 m |
58 ft 5 in |
height |
3.9 m |
12 ft 10 in |
50.39 m |
165 ft 4 in |
wingspan |
7.7 m |
25 ft 3 in |
3x GE CF6-50C Turbofan |
engines |
Two General Electric J85-GE-5A turbojet engines |
54,000 lbf |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
162,000 lbf |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
251,744 kg |
555,000 lb |
MTOW |
12,093 lb |
5,485 kg |
9,630 km |
5,200 nm |
range |
1,759 km |
950 nm |
507 knots |
939 km/h |
cruise speed |
745 kts |
1,380 km/h |
Up to 380 passengers |
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.