Cessna A-37 Dragonfly vs. Airbus H225 Super Puma
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Cessna A-37 Dragonfly |
versus |
Airbus H225 Super Puma |
8.617 m |
28 ft 3 in |
length |
14.06 m |
46 ft 2 in |
2.71 m |
8 ft 11 in |
height |
4.38 m |
14 ft 4 in |
10.94 m |
35 ft 11 in |
wingspan |
|
|
2 x General Electric J85-GE-17A turbojets |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
2,850 lbs |
thrust per engine |
2,778 hp |
2 x 2,850 lbs = 5,700 lbs |
total thrust |
5,556 hp |
6,350 kg |
14,000 lb |
MTOW |
11,000 kg |
24,251 lb |
460 nmi |
852 km |
range |
857 km |
463 nm |
489 mph |
787 km/h |
cruise speed |
242 km/h |
150 mph |
3,000 pounds of bombs, rockets and missiles |
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.