McDonnell Douglas A-4 Skyhawk vs. Airbus H225 Super Puma

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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.