Folland Gnat vs. Airbus H225 Super Puma

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Folland Gnat versus Airbus H225 Super Puma
9.67 m 31 ft 9 in length 14.06 m 46 ft 2 in
2.95 m 9 ft 8 in height 4.38 m 14 ft 4 in
7.32 m 24 ft wingspan
Bristol Siddeley Orpheus 100 engines 2 x Turbomeca Makila 2A turboshaft engines
4700 lbf thrust per engine 2,778 hp
4700 lbf total thrust 5,556 hp
3,915 kg 8,630 lb MTOW 11,000 kg 24,251 lb
1,851 km 999 nm range 857 km 463 nm
360 mph 579 km/h cruise speed 242 km/h 150 mph
Single or two-seat light fighter and trainer aircraft 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.