McDonnell Douglas A-4 Skyhawk vs. Airbus H225 Super Puma
... or view the full comparison list
here.
McDonnell Douglas A-4 Skyhawk |
versus |
Airbus H225 Super Puma |
12.19 m |
40 ft 0 in |
length |
14.06 m |
46 ft 2 in |
4.57 m |
15 ft |
height |
4.38 m |
14 ft 4 in |
8.08 m |
26 ft 6 in |
wingspan |
|
|
1x Pratt & Whitney J52-P-6A Jet |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
8,500 pound-force |
thrust per engine |
2,778 hp |
8,500 pound-force |
total thrust |
5,556 hp |
11,113 kg |
24,500 lb |
MTOW |
11,000 kg |
24,251 lb |
3,222 km |
1,739 nm |
range |
857 km |
463 nm |
586 kts |
364 mph |
cruise speed |
242 km/h |
150 mph |
Up to 9,155 pounds of weapons on 5 hardpoints |
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.