McDonnell-Douglas DC-9-30 vs. Northrop T-38 Talon
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McDonnell-Douglas DC-9-30 |
versus |
Northrop T-38 Talon |
36.36 m |
119 ft 3 in |
length |
14.1 m |
46 ft 4 in |
8.5 m |
27 ft 11 in |
height |
3.9 m |
12 ft 10 in |
28.44 m |
93 ft 4 in |
wingspan |
7.7 m |
25 ft 3 in |
2x Pratt & Whitney JT8D |
engines |
Two General Electric J85-GE-5A turbojet engines |
15,000 pound-force |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
30,000 pound-force (2 engines) |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
54,885 kg |
121,000 lb |
MTOW |
12,093 lb |
5,485 kg |
2,632 km |
1,422 nm |
range |
1,759 km |
950 nm |
898 km/h |
558 mph |
cruise speed |
745 kts |
1,380 km/h |
Up to 139 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.