Northrop T-38 Talon vs. AgustaWestland AW109
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Northrop T-38 Talon |
versus |
AgustaWestland AW109 |
14.1 m |
46 ft 4 in |
length |
13,04 m |
42 ft 9 in |
3.9 m |
12 ft 10 in |
height |
3,40 m |
11 ft 2 in |
7.7 m |
25 ft 3 in |
wingspan |
|
|
Two General Electric J85-GE-5A turbojet engines |
engines |
2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
638 shp (476 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
1276 shp (952 kW) |
12,093 lb |
5,485 kg |
MTOW |
3,175 kg |
7,000 lb |
1,759 km |
950 nm |
range |
932 km |
503 nm |
745 kts |
1,380 km/h |
cruise speed |
285 km/h |
177 mph |
Two (student and instructor) |
capacity |
1 or 2 pilots + up to 7 passengers |
|
|
rotor diameter |
11.00 m |
36 ft 1 in |
|
|
rate of climb |
651 m/min |
2,136 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.