Lockheed Martin F-35 Lightning II vs. Airbus H225 Super Puma

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Lockheed Martin F-35 Lightning II versus Airbus H225 Super Puma
15.67 m 51 ft 4 in length 14.06 m 46 ft 2 in
4.33 m 14 ft 2 in height 4.38 m 14 ft 4 in
10.7 m 35 ft 1 in wingspan
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 2 x Turbomeca Makila 2A turboshaft engines
40,000 lb thrust per engine 2,778 hp
40,000 lb total thrust 5,556 hp
31,800 kg 70,000 lb MTOW 11,000 kg 24,251 lb
1,380 mi 1,200 nm range 857 km 463 nm
520 kt 302 mph cruise speed 242 km/h 150 mph
18,000 pounds of total ordinance 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.