| The Super Puma is well suited for
multi mission application.
Designed to last out century, the Super Puma owes the above
qualities of safety, operational efficiency, versatility, economy and comfort to the
incorporation of the very latest technology, it is thus the fruit of through research,
applied to the following areas :
-
Using more composite materials
-
High engine efficiency, low fuel consumption
-
Rotor-head frequency adapters
-
Modular design for main power train assemblies
-
Simplified maintenance with the TBOs
-
Newly designed systems
With its blend of new technologies, the Super Puma embodies
all the qualities expected of a modern helicopter, in terms both of performance and of
operational characteristic.
The Super Puma Military version,
suitability for Modern Combat Conditions
The Super Puma Military version helicopter is a multi
purpose twin engine transport helicopter for :
-
Utility Version (no armament capability)
-
Utility + Armament capability (canons, machine guns,
rockets)
The Super Puma Naval Mission, is The True Multi-role Naval
Helicopter
In order to achieve in the most efficient way maritime
surveillance of wide areas, early warning for naval task force, anti surface and anti
submarine warfare, the Super Puma is equipped with a sophisticated electronic package,
associating the latest generation sensor with power computing equipment.
PERFORMANCE
Performance on 2 engine
|
|
| Max. Speed Vne |
278 |
km/hr |
50 |
kts |
278 |
km/hr |
150 |
kts |
| Fast Cruise
Speed |
258 |
km/hr |
139 |
kts |
262 |
km/hr |
141 |
kts |
| Economical
Cruise Speed |
248 |
km/hr |
134 |
kts |
252 |
km/hr |
136 |
kts |
Fuel
Consumption at
Economical Cruise Speed |
510 |
kg/hr |
1,124 |
lb./h |
502 |
kg/hr |
1,107 |
lb./h |
| Rate of Climb
at 70 kts |
7.2 |
m/sec |
1,417 |
ft/min |
8.2 |
m/sec |
1,618 |
ft/min |
| Hover
Ceiling IGE (10 ft) |
| - ISA |
2,800 |
m |
9,196 |
ft |
3,250 |
m |
10,663 |
ft |
| - ISA +
20 degree C |
1,800 |
m |
5,906 |
ft |
2,300 |
m |
7,546 |
ft |
| Hover
Ceiling OGE |
| - ISA |
1,650 |
m |
5,413 |
ft |
2,300 |
m |
7,546 |
ft |
| - ISA +
20 degree C |
850 |
m |
2,789 |
ft |
1,400 |
m |
4,593 |
ft |
|
| WEIGHT |
NAS-332 C1 |
NAS-332 L1 |
|
| Max. Take Off
Weight |
9,000
kg |
19,840
lbs |
8,600
kg |
18,960
lbs |
| Empty Weight |
4,330
kg |
9,546
lbs |
4,460
kg |
9,832
lbs |
| Useful Load |
4,670
kg |
10,294
lbs |
4,140
kg |
9,128
lbs |
| Max. Gross
Weight |
9,000
kg |
19,840
lbs |
8,600
kg |
18,960
lbs |
Max. Gross
Weight in
External Load |
9,350 kg |
20,615 lbs |
9,350 kg |
20,615 lbs |
| Max. Cargo
Sling Load |
4,500
kg |
9,920
lbs |
4,500
kg |
9,920
lbs |
|
|