North American F-100 Super Sabre vs. Airbus H225 Super Puma
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here.
North American F-100 Super Sabre |
versus |
Airbus H225 Super Puma |
16.46 m |
54 ft 2 in |
length |
14.06 m |
46 ft 2 in |
4.93 m |
16 ft 2 in |
height |
4.38 m |
14 ft 4 in |
11.84 m |
38 ft 1 |
wingspan |
|
|
1 Pratt & Whitney J57-P-21A |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
16,000 lb. thrust in afterburner |
thrust per engine |
2,778 hp |
16,000 lb. (afterburner) |
total thrust |
5,556 hp |
17,609 kg |
38,800 lb |
MTOW |
11,000 kg |
24,251 lb |
2,673 km |
1,444 nm |
range |
857 km |
463 nm |
587 mph |
945 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.