Sukhoi SSJ 100 95LR vs. Northrop T-38 Talon
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Sukhoi SSJ 100 95LR |
versus |
Northrop T-38 Talon |
29.94 m |
98 ft 2 in |
length |
14.1 m |
46 ft 4 in |
10.28 m |
33 ft 8 in |
height |
3.9 m |
12 ft 10 in |
27.8 m |
91 ft 2 in |
wingspan |
7.7 m |
25 ft 3 in |
2 PowerJet SaM146 turbofans |
engines |
Two General Electric J85-GE-5A turbojet engines |
15,400 (68.5 KN) to 16,100 (71.6 KN) at NTO, 17,500 (77.9 KN) to 17,800 (79.2 KN) with APR |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
30,800 (137 KN) to 32,200 (143.2 KN) at NTO, 35,000 (155.8 KN) to 35,600 (158.4 KN) with APR |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
49,450 kg |
109,000 lb |
MTOW |
12,093 lb |
5,485 kg |
4,578 km |
2,470 nm |
range |
1,759 km |
950 nm |
515 mph |
830 km/h |
cruise speed |
745 kts |
1,380 km/h |
98 (up to 108) 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.