Lockheed T-33 Shooting Star vs. Airbus H225 Super Puma
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Lockheed T-33 Shooting Star |
versus |
Airbus H225 Super Puma |
11.51 m |
37 ft 9 in |
length |
14.06 m |
46 ft 2 in |
3.56 m |
11 ft 8 in |
height |
4.38 m |
14 ft 4 in |
11.9 m |
39 ft 1 in |
wingspan |
|
|
1 (Allison J33-A-5) |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
24.0 kN |
thrust per engine |
2,778 hp |
24.0 kN |
total thrust |
5,556 hp |
5,900 kg |
13,000 lb |
MTOW |
11,000 kg |
24,251 lb |
2,050 km |
1,107 nm |
range |
857 km |
463 nm |
965 km/h |
600 mph |
cruise speed |
242 km/h |
150 mph |
907 kg of bombs or rockets |
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.