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.