Murphy Moose: Difference between revisions
lead para reworked |
No edit summary |
||
Line 1: | Line 1: | ||
{{Citations missing|article|date=August 2011}} |
|||
__NOTOC__ |
__NOTOC__ |
||
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
Revision as of 16:25, 22 August 2011
This article needs additional citations for verification. (August 2011) |
Murphy Moose | |
---|---|
A radial-equipped Murphy Moose | |
Role | Kit aircraft |
National origin | Canada |
Manufacturer | Murphy Aircraft |
The Murphy Moose is a Canadian high-wing utility light aircraft produced in kit form by Murphy Aircraft of Chilliwack, British Columbia for amateur construction. 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- tailwheel undercarriage)
Data from Jane's All The World's Aircraft 2003–2004[1]
General characteristics
- Crew: 1
- Capacity: 5 passengers
- Length: 7.01 m (23 ft 0 in)
- Wingspan: 10.97 m (36 ft 0 in)
- Height: 1.98 m (6 ft 6 in)
- Wing area: 16.91 m2 (182.0 sq ft)
- Empty weight: 816 kg (1,799 lb)
- Gross weight: 1,587 kg (3,499 lb)
- Powerplant: 1 × Vedeneyev M14P 9-cylinder radial engine, 265 kW (355 hp)
Performance
- Maximum speed: 282 km/h (175 mph, 152 kn)
- Cruise speed: 249 km/h (155 mph, 134 kn) (70% power)
- Stall speed: 81 km/h (50 mph, 44 kn) (flaps down)
- Never exceed speed: 304 km/h (189 mph, 164 kn)
- Range: 965 km (600 mi, 521 nmi) (standard fuel)
- Service ceiling: 4,575 m (15,010 ft)
- Rate of climb: 7.6 m/s (1,500 ft/min)
See also
Related development
Aircraft of comparable role, configuration, and era
References
- ^ Jackson 2003, p. 66.
- Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.