BAC Jet Provost vs. Airbus H225 Super Puma

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BAC Jet Provost versus Airbus H225 Super Puma
10.36 m 34 ft 0 in length 14.06 m 46 ft 2 in
3.1 m 10 ft 2 in height 4.38 m 14 ft 4 in
11.25 m 36 ft 11 in wingspan
1 x Bristol Siddeley Viper 201 engines 2 x Turbomeca Makila 2A turboshaft engines
2,500 lb = 1,134 kg thrust per engine 2,778 hp
2,500 lb = 1,134 kg total thrust 5,556 hp
4,173 kg 9,200 lb MTOW 11,000 kg 24,251 lb
1,448 km 782 nm range 857 km 463 nm
440 mph 708 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.