North American T-2 Buckeye vs. Airbus H225 Super Puma

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North American T-2 Buckeye versus Airbus H225 Super Puma
11.67 m 38 ft 4 in length 14.06 m 46 ft 2 in
4.51 m 14 ft 10 in height 4.38 m 14 ft 4 in
11.62 m 38 ft 1 in wingspan
Two General Electric J85-GE-4 turbojet engines engines 2 x Turbomeca Makila 2A turboshaft engines
2,950 lbf thrust per engine 2,778 hp
5,900 lbf total thrust 5,556 hp
13,179 lb 5,977 kg MTOW 11,000 kg 24,251 lb
1,685 km 909 nm range 857 km 463 nm
453 kts 281 mph cruise speed 242 km/h 150 mph
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.