Bombardier CS100 vs. Northrop T-38 Talon
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Bombardier CS100 |
versus |
Northrop T-38 Talon |
35.00 m |
114 ft 10 in |
length |
14.1 m |
46 ft 4 in |
11.5 m |
37 ft 9 in |
height |
3.9 m |
12 ft 10 in |
35.1 m |
115 ft 2 in |
wingspan |
7.7 m |
25 ft 3 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
Two General Electric J85-GE-5A turbojet engines |
84.1 kN |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
168.2 kN |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
54,931 kg |
121,100 lb |
MTOW |
12,093 lb |
5,485 kg |
4,074 km |
2,200 nm |
range |
1,759 km |
950 nm |
871 km/h |
541 mph |
cruise speed |
745 kts |
1,380 km/h |
110 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.