CH-149 Cormorant: Difference between revisions

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|align="left"|<div style="font-size: 80%">[[Length:]] 22.8 m</div>
|align="left"|<div style="font-size: 80%">Length: 22.8 m</div>
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|align="left"|<div style="font-size: 80%">[[Rotor span:]] 18.5 m</div>
|align="left"|<div style="font-size: 80%">Rotor span: 18.5 m</div>
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|align="left"|<div style="font-size: 80%">[[Height:]] 6.5 m</div>
|align="left"|<div style="font-size: 80%">Height: 6.5 m</div>
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|align="left"|<div style="font-size: 80%">[[Weight]] 14,600 kg</div>
|align="left"|<div style="font-size: 80%">Weight 14,600 kg</div>
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|align="left"|<div style="font-size: 80%">[[Engine:]] 3 General Electric T700-T6A1 Turbines  </div>
|align="left"|<div style="font-size: 80%">Engine: 3 General Electric T700-T6A1 Turbines  </div>
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|align="left"|<div style="font-size: 80%">[[Speed:]] 278 km/h</div>
|align="left"|<div style="font-size: 80%">Speed: 278 km/h</div>
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|align="left"|<div style="font-size: 80%">[[Range: ]]1,018 km</div>
|align="left"|<div style="font-size: 80%">Range: 1,018 km</div>
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|align="left"|<div style="font-size: 80%">[[Years Procured:]] 2001 to 2003</div>
|align="left"|<div style="font-size: 80%">Years Procured: 2001 to 2003</div>
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|align="left"|<div style="font-size: 80%">[[Quantity:]] 15</div>
|align="left"|<div style="font-size: 80%">Quantity: 15</div>


[http://www.airforce.forces.gc.ca/equip/ch-149/intro_e.asp]
[http://www.airforce.forces.gc.ca/equip/ch-149/intro_e.asp]

Latest revision as of 22:19, 2 December 2006

CH-149
Length: 22.8 m
Rotor span: 18.5 m
Height: 6.5 m
Weight 14,600 kg
Engine: 3 General Electric T700-T6A1 Turbines
Speed: 278 km/h
Range: 1,018 km
Years Procured: 2001 to 2003
Quantity: 15

[1]

The Agusta-Westland CH-149 Cormorant, is a fully certified off-the-shelf civilian utility helicopter. It has been modified from the military specifications of the EH-101 to include search and rescue-specific equipment and physical characteristics and performance requirements to meet Canada’s SAR responsibilities. This modification provided reduced procurement costs, a rear-fuselage ramp, a single rescue door with both hoists on one side, and eliminated unnecessary military equipment.

Shaped rotor blades, strengthened by titanium strips along the leading edge, allow the CH-149 to improve lift and increase speed, lowering the stall speed and reducing vibration. This enables it to withstand high winds (exceeding 50 knots), provide superior gust response while carrying out routine tasks of hoisting, starting and stopping.

[2]