Boeing 717-200HGW vs. Northrop T-38 Talon
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Boeing 717-200HGW |
versus |
Northrop T-38 Talon |
37.80 m |
123 ft 11 in |
length |
14.1 m |
46 ft 4 in |
8.87 m |
29 ft 1 in |
height |
3.9 m |
12 ft 10 in |
28.44 m |
93 ft 4 in |
wingspan |
7.7 m |
25 ft 3 in |
2 Rolls-Royce BR715 |
engines |
Two General Electric J85-GE-5A turbojet engines |
82.3kN (18,500lb) to 93.4kN (21,000lb) |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
164.6kN (37,000lb) to 186.8kN (42,000lb) |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
54,885 kg |
121,000 lb |
MTOW |
12,093 lb |
5,485 kg |
2,060 nm |
3,814 km |
range |
1,759 km |
950 nm |
811 km/h |
504 mph |
cruise speed |
745 kts |
1,380 km/h |
106 passengers in a 2 class configuration |
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.