Lockheed F-104 Starfighter vs. Airbus H225 Super Puma
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Lockheed F-104 Starfighter |
versus |
Airbus H225 Super Puma |
16.69 m |
54 ft 9 in |
length |
14.06 m |
46 ft 2 in |
4.11 m |
13 ft 6 in |
height |
4.38 m |
14 ft 4 in |
6.68 m |
21 ft 11 in |
wingspan |
|
|
1 Turbojet Engine |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
46.7 / 71.2 kN (dry/with Afterburner) |
thrust per engine |
2,778 hp |
46.7 / 71.2 kN (dry/with Afterburner) |
total thrust |
5,556 hp |
13,500 kg |
29,800 lb |
MTOW |
11,000 kg |
24,251 lb |
1,200 km |
648 nm |
range |
857 km |
463 nm |
510 mph |
821 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.