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Revision as of 08:35, 8 May 2019 editCydebot (talk | contribs)6,812,251 editsm Robot - Moving category United States sailplanes 1970–1979 to Category:1970s United States sailplanes per CFD at Misplaced Pages:Categories for discussion/Log/2019 April 19.← Previous edit Revision as of 13:39, 16 April 2020 edit undo192.80.55.86 (talk) Specifications (Monerai S): added additional specs from http://www.monerai.com/specifications.htmlNext edit →
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|height ft=4 |height ft=4
|height in=4 |height in=4
|wing area sqm= |wing area sqm=7.25
|wing area sqft= |wing area sqft=78
|swept area sqm=<!-- swing-wings --> |swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings --> |swept area sqft=<!-- swing-wings -->
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|volume m3=<!-- lighter-than-air --> |volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air -->
|aspect ratio=<!-- sailplanes --> |aspect ratio=16.6:1
|empty weight kg=100 |empty weight kg=100
|empty weight lb=220 |empty weight lb=220
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|ceiling m= |ceiling m=
|ceiling ft= |ceiling ft=
|glide ratio=<!-- sailplanes -->28 |glide ratio=<!-- sailplanes -->28:1 at 60mph
|climb rate ms= |climb rate ms=
|climb rate ftmin= |climb rate ftmin=
|sink rate ms=<!-- sailplanes -->0.85 |sink rate ms=<!-- sailplanes -->0.85
|sink rate ftmin=<!-- sailplanes -->167 |sink rate ftmin=<!-- sailplanes -->at 55mph: 167
|armament1= |armament1=
|armament2= |armament2=

Revision as of 13:39, 16 April 2020

Monerai
Monerai S
Role SailplaneType of aircraft
National origin United States
Manufacturer Monnett Experimental Aircraft
Designer John Monnett
First flight Template:Avyear
Introduction 1978
Number built 100 by January 1984 from 375 kits sold.

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 pod-and-boom fuselage consists of a welded steel tube truss encased in a fiberglass shell, with an aluminum tube for the tailboom. 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.

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 22 hp (16 kW) Zenoah G-25 or the 25 hp (19 kW) KFM 107 engine.
Monerai Max
Monerai P version with extended wing tips

Aircraft on display

Specifications (Monerai S)

General characteristics

Performance

  • Maximum glide ratio: 28:1 at 60mph

References

  1. Moll, Nigel; Comstock, Bryan (May 1983). "Monerai Service Bulletin". Reporting Points. Flying. Vol. 110, no. 5. Ziff Davis. p. 12. ISSN 0015-4806. Retrieved 15 August 2016 – via Google Books.
  2. John Monnett (Oct 1977). "Try a new flavor... the Monerai". Sport Aviation.
  3. ^ Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 123. Soaring Society of America, November 1983. USPS 499-920
  4. US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.
  5. http://neam.org/index.php?option=com_content&view=article&id=870
  • Jane's All the World's Aircraft 1985-86. p. 756.

External links

Aircraft designed by John Monnett
Aircraft
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