Boeing 757-200 vs. Airbus H225 Super Puma
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Boeing 757-200 |
versus |
Airbus H225 Super Puma |
47.3 m |
155 ft 2 in |
length |
14.06 m |
46 ft 2 in |
13.56 m |
44 ft 6 in |
height |
4.38 m |
14 ft 4 in |
38.1 m |
125 ft |
wingspan |
|
|
Rolls-Royce RB211 or Pratt & Whitney PW2000 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
36,600–43,500 lbf (163–193 kN) |
thrust per engine |
2,778 hp |
77,000 to 80,000 pounds |
total thrust |
5,556 hp |
115,666 kg |
255,000 lb |
MTOW |
11,000 kg |
24,251 lb |
6,300 km |
3,400 nm |
range |
857 km |
463 nm |
876 km/h |
544 mph |
cruise speed |
242 km/h |
150 mph |
200 passengers |
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.