Polikarpov I-16 vs. Airbus H225 Super Puma
... or view the full comparison list
here.
Polikarpov I-16 |
versus |
Airbus H225 Super Puma |
6.13 m |
20 ft 1 in |
length |
14.06 m |
46 ft 2 in |
3.25 m |
10 ft 8 in |
height |
4.38 m |
14 ft 4 in |
9 m |
29 ft 6 in |
wingspan |
|
|
1x Shvetsov M-25 radial engine |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1000 hp |
thrust per engine |
2,778 hp |
1000 hp |
total thrust |
5,556 hp |
2,060 kg |
4,540 lb |
MTOW |
11,000 kg |
24,251 lb |
248 mi |
216 nm |
range |
857 km |
463 nm |
180 mph |
290 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.