McDonnell Douglas F-4 Phantom II vs. Airbus H225 Super Puma

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McDonnell Douglas F-4 Phantom II versus Airbus H225 Super Puma
19.2 m 63 ft 0 in length 14.06 m 46 ft 2 in
5.03 m 16 ft 6 in height 4.38 m 14 ft 4 in
11.72 m 38 ft 5 in wingspan
Two General Electric J79s engines 2 x Turbomeca Makila 2A turboshaft engines
17,900 lbs thrust per engine 2,778 hp
35,800 lbs total thrust 5,556 hp
27,965 kg 61,700 lb MTOW 11,000 kg 24,251 lb
3,031 km 1,636 nm range 857 km 463 nm
Mach 2.2 2,717 km/h cruise speed 242 km/h 150 mph
Up to 16,000 lbs of externally carried ordnance 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.