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Monnett Monerai : ウィキペディア英語版
Monnett Monerai
__NOTOC__

The Monnett Monerai is a sailplane that was developed in the United States in the late 1970s for homebuilding. It is a conventional pod-and-boom design with a V-tail and a mid-mounted cantilever wing of constant chord.
The kit assembles in approximately 600 hours. It has bonded wing skins and incorporates 90° flaps for glide path control. The fuselage is of steel tube construction encased in a fiberglass shell. A spar fitting modification was released in 1983.
A powered version was designed as the Monerai P with an engine mounted on a pylon above the wings. A Sachs Rotary Engine was chosen for the prototype. A version with extended wing tips is also available (Monerai Max) which increases the span to 12 m (39 ft) and raises the glide ratio from 28:1 to more than 30:1.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 123. Soaring Society of America, November 1983. USPS 499-920〕
Both the powered Monerai P and the unpowered Monerai S versions are identical structurally.


==Variants==
;Monerai S
:unpowered glider
;Monerai P
:powered glider equipped with the Zenoah G-25 or the KFM 107 engine.〔
;Monerai Max
:Monerai P version with extended wing tips〔

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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