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[[Image:murphy moose.jpg|thumb|A radial-equipped Murphy Moose.]]
{|{{Infobox Aircraft Begin
| name=Murphy Moose
| image=Image:murphy moose.jpg
| caption=A radial-equipped Murphy Moose
}}{{Infobox Aircraft Type
| type=[[Homebuilt aircraft|Kit aircraft]]
| national origin=[[Canada]]
| manufacturer=[[Murphy Aircraft]]
| designer=
| first flight=
| introduced=
| retired=
| status=
| primary user=
| more users= <!--Limited to three in total; separate using <br /> -->
| produced= <!--years in production-->
| number built=
| program cost= <!--Total program cost-->
| unit cost= <!--Incremental or flyaway cost for military or retail price for commercial aircraft-->
| developed from=
| variants with their own articles=
}}
|}
[[Image:MurphyMooseUnderConstruction.JPG|thumb|right|Inside of the tail cone of a Murphy Moose under construction, showing the [[semi-monocoque]] design]]
[[Image:MurphyMooseUnderConstruction.JPG|thumb|right|Inside of the tail cone of a Murphy Moose under construction, showing the [[semi-monocoque]] design]]



Revision as of 22:04, 3 October 2010

Murphy Moose
A radial-equipped Murphy Moose
Role Kit aircraft
National origin Canada
Manufacturer Murphy Aircraft
Inside of the tail cone of a Murphy Moose under construction, showing the semi-monocoque design

The Murphy Moose is a large high-wing utility monoplane designed to handle nearly any airfield under any conditions. A homebuilt kit aircraft, the Moose can be purchased as a "quick-build" kit which comes partly pre-assembled. Similar in many respects to the de Havilland Canada DHC-2 Beaver, the Moose is cheaper both to buy and to operate.

Builders can choose whether to equip their aircraft with the 269 kW (360 hp) Russian-built Vedeneyev M14P 9-cylinder radial, or the horizontally-opposed 187 kW (250 hp) Lycoming O-540. Both engines allow the Moose to take off in roughly 180 m (600 ft).

Specifications (Moose M-14P)

General characteristics

  • Crew: one pilot
  • Capacity: 3-5 passengers
  • Length: 8.43 m (25 ft 8 in)
  • Wingspan: 11.05 m (36 ft 3 in)
  • Wing area: 16.9 m² (182 ft²)
  • Empty: 816 kg (1,800 lb)
  • Loaded: 1,586 kg (3,500 lb)
  • Powerplant:Vedeneyev M14P supercharged 9-cylinder radial engine, 269 kW (360 hp)

Performance

  • Maximum speed: 281 km/h (175 mph)
  • Range: 1,840 km (1,150 miles)
  • Rate of climb: 458 m/min (1,500 ft/min)
  • Wing loading: 94 kg/m² (19 lb/ft²)
  • Power/Mass: 0.17 kW/kg (0.10 hp/lb)

See also

Related development

Aircraft of comparable role, configuration, and era

References

  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.