Northrop T-38 Talon vs. Mil Mi-26
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Northrop T-38 Talon |
versus |
Mil Mi-26 |
14.1 m |
46 ft 4 in |
length |
40.03 m |
131.3 ft |
3.9 m |
12 ft 10 in |
height |
8.15 m |
26.7 ft |
7.7 m |
25 ft 3 in |
wingspan |
|
|
Two General Electric J85-GE-5A turbojet engines |
engines |
2 x Lotarev D-136 turboshaft engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
8,380 kW |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
16,760 kW |
12,093 lb |
5,485 kg |
MTOW |
56,000 kg |
123,459 lb |
1,759 km |
950 nm |
range |
800 km |
432 nm |
745 kts |
1,380 km/h |
cruise speed |
255 km/h |
158 mph |
Two (student and instructor) |
capacity |
Up to 90 passengers |
|
|
rotor diameter |
32.00 m |
105 ft 0 in |
|
|
rate of climb |
8 m/s |
1,574 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.