Lockheed L-1011 TriStar 500 vs. Airbus H225 Super Puma
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Lockheed L-1011 TriStar 500 |
versus |
Airbus H225 Super Puma |
50.05 m |
164 ft 3 in |
length |
14.06 m |
46 ft 2 in |
16.87 m |
55 ft 4 in |
height |
4.38 m |
14 ft 4 in |
50.09 m |
164 ft 4 in |
wingspan |
|
|
3 Rolls-Royce RB211 engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
42,000 lbf |
thrust per engine |
2,778 hp |
126,000 lbf (3 engines x 42,000 lbf per engine) |
total thrust |
5,556 hp |
231,330 kg |
510,000 lb |
MTOW |
11,000 kg |
24,251 lb |
11,260 km |
6,100 nm |
range |
857 km |
463 nm |
525 knots |
972 km/h |
cruise speed |
242 km/h |
150 mph |
Max. 315 passengers (typical 253) |
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.