de Havilland Venom vs. Airbus H225 Super Puma

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de Havilland Venom versus Airbus H225 Super Puma
6.71 m 22 ft 0 in length 14.06 m 46 ft 2 in
1.88 m 6 ft 2 in height 4.38 m 14 ft 4 in
12.7 m 41 ft 8 in wingspan
1 (de Havilland Ghost 105) engines 2 x Turbomeca Makila 2A turboshaft engines
23.6 kN thrust per engine 2,778 hp
23.6 kN total thrust 5,556 hp
6,945 kg 15,300 lb MTOW 11,000 kg 24,251 lb
1,730 km 935 nm range 857 km 463 nm
1030 km/h 640 mph 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.