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Wood Sky Pup : ウィキペディア英語版
Wood Sky Pup

The Wood Sky Pup is an American single-seat, high wing, cantilever, single engine, conventional landing gear ultralight aircraft that was designed by Steven K. Wood of Whitewater, Colorado for amateur construction.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page B-54. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕〔Downey, Julia: ''2001 Plans Aircraft Directory'', Kitplanes, Volume 18, Number 1, January 2001, page 31. Kitplanes Acquisition Company. ISSN 0891-1851〕〔Downey, Julia: ''2002 Plans Aircraft Directory'', Kitplanes, Volume 19, Number 1, January 2002, page 31. Kitplanes Acquisition Company. ISSN 0891-1851〕〔Downey, Julia: ''2003 Plans Aircraft Directory'', Kitplanes, Volume 20, Number 1, January 2003, page 30. Primedia Publications. ISSN 0891-1851〕
==Design and development==
Introduced in 1982, the Sky Pup is a single seater designed as an FAR 103 Ultralight Vehicles compliant aircraft with an empty weight within that category's empty weight limit. The aircraft was intended to require the minimum financial investment and the designer intended that the airframe would be able to be completed for US$1000 using locally available materials. Cliche reported in 2001 that Sky Pups had been completed for US$2000, including the engine.〔〔
The aircraft fuselage and wings are constructed from epoxy-glued Douglas fir, with foam wing ribs all covered in doped fabric or Dacron. The wing is a three-piece design, allowing quick disassembly for transport or storage. The landing gear suspension is made from maple wood. The Sky Pup can be built with an open cockpit or fully enclosed, allowing flying in cooler weather. The Sky Pup is available as plans only. The power range specified is , with the largest engine specified the Rotax 277. The 2si 215, Hirth F-33 and Zenoah G-25 have also been used.〔〔
The design was professionally engineered and incorporates a very clean cantilever wing that results in a 12:1 glide ratio. The control system is two-axis, using only elevator and rudder controls, roll being introduced by rudder via a generous dihedral angle. The elevator is stick-controlled, while the rudder is controlled via conventional aircraft pedals. The aircraft is stall and spin proof. Reported construction times are 450–600 hours.〔〔
Plans were initially sold direct by the designer and, in the early 2000s, by the Vintage Ultra and Lightplane Association. Later the designer's son marketed the plans and this is the current source.〔〔〔〔〔



抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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