CASA 2.111 vs. Northrop T-38 Talon
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CASA 2.111 |
versus |
Northrop T-38 Talon |
16.4 m |
53 ft 10 in |
length |
14.1 m |
46 ft 4 in |
3.9 m |
12 ft 10 in |
height |
3.9 m |
12 ft 10 in |
22.5 m |
73 ft 1 |
wingspan |
7.7 m |
25 ft 3 in |
2 × Rolls-Royce Merlin 500-29 V-12 liquid-cooled piston engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
1,176 kW (1,577 hp) |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
2,352 kW (3,154 hp) |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
14,000 kg |
30,900 lb |
MTOW |
12,093 lb |
5,485 kg |
1,950 km |
1,053 nm |
range |
1,759 km |
950 nm |
315 km/h |
196 mph |
cruise speed |
745 kts |
1,380 km/h |
|
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.