Northrop T-38 Talon vs. Airbus H225 Super Puma

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Northrop T-38 Talon versus Airbus H225 Super Puma
14.1 m 46 ft 4 in length 14.06 m 46 ft 2 in
3.9 m 12 ft 10 in height 4.38 m 14 ft 4 in
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines 2 x Turbomeca Makila 2A turboshaft engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 2,778 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust 5,556 hp
12,093 lb 5,485 kg MTOW 11,000 kg 24,251 lb
1,759 km 950 nm range 857 km 463 nm
745 kts 1,380 km/h cruise speed 242 km/h 150 mph
Two (student and instructor) capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.