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