Lockheed U-2 vs. Airbus H225 Super Puma

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Lockheed U-2 versus Airbus H225 Super Puma
19.2 m 63 ft 0 in length 14.06 m 46 ft 2 in
4.8 m 15 ft 9 in height 4.38 m 14 ft 4 in
32 m 105 ft wingspan
1 × General Electric F118-101 engines 2 x Turbomeca Makila 2A turboshaft engines
17,000 lbf (76 kN) thrust per engine 2,778 hp
17,000 lbf (76 kN) total thrust 5,556 hp
18,144 kg 40,000 lb MTOW 11,000 kg 24,251 lb
6,090 nm 11,278 km range 857 km 463 nm
475 mph 764 km/h 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.