Lockheed Martin F-22 Raptor vs. Airbus H225 Super Puma
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Lockheed Martin F-22 Raptor |
versus |
Airbus H225 Super Puma |
18.9 m |
62 ft 1 in |
length |
14.06 m |
46 ft 2 in |
5.1 m |
16 ft 9 in |
height |
4.38 m |
14 ft 4 in |
13.6 m |
44 ft 7 in |
wingspan |
|
|
Two Pratt & Whitney F119-PW-100 turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
35,000-pound class |
thrust per engine |
2,778 hp |
70,000-pound class |
total thrust |
5,556 hp |
38,000 kg |
83,500 lb |
MTOW |
11,000 kg |
24,251 lb |
1,850 mi |
1,611 nm |
range |
857 km |
463 nm |
Mach 1.6 |
1976 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.