Boeing F/A-18E/F Super Hornet vs. Airbus H225 Super Puma
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here.
| Boeing F/A-18E/F Super Hornet |
versus |
Airbus H225 Super Puma |
| 18.5 m |
60 ft 3 in |
length |
14.06 m |
46 ft 2 in |
| 4.87 m |
16 ft |
height |
4.38 m |
14 ft 4 in |
| 13.68 m |
44 ft 1 |
wingspan |
|
|
| Two F414-GE-400 turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
| Up to 17,000 lbs |
thrust per engine |
2,778 hp |
| Up to 34,000 lbs |
total thrust |
5,556 hp |
| 29,937 kg |
66,000 lb |
MTOW |
11,000 kg |
24,251 lb |
| 2,346 km |
1,268 nm |
range |
857 km |
463 nm |
| 1032 knots |
1,911 km/h |
cruise speed |
242 km/h |
150 mph |
| Overall capability across all eleven hardpoints is 17,750lbs of external stores |
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.
