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__NOTOC__ | |||
<!-- This article is a part of ]. Please see ] for recommended layout. --> | <!-- This article is a part of ]. Please see ] for recommended layout. --> | ||
{{Infobox aircraft | |||
| name= | | name=Monerai | ||
| image= | | image=MONERAI-S.jpg | ||
| caption= | | caption=Monerai S | ||
| type=Sailplane | |||
}}{{Infobox Aircraft Type | |||
| national_origin=United States | |||
| type= | |||
| manufacturer=] | |||
| national origin= | |||
| designer=] | |||
| manufacturer= | |||
| first_flight= 1978 | |||
| designer= | |||
| introduction=1978 | |||
| first flight= | |||
| introduced= | |||
| retired= | | retired= | ||
| status= | | status= | ||
| |
| primary_user= | ||
| number_built=100 by January 1984 from 375 kits sold | |||
| number built= | |||
| |
| developed_from= | ||
| variants |
| variants= | ||
}} | }} | ||
|} | |||
The '''Monnett Monerai''' is a ] that was developed in the United States in the late 1970s for ]. It is a conventional pod-and-boom design with a ] and a mid-mounted cantilever wing of constant chord. | |||
<!-- ==Development== --> | |||
The kit assembles in approximately 600 hours. It has bonded wing skins and incorporates 90° ]s 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.<ref name="FlyingMay1983">{{cite magazine|last1=Moll|first1=Nigel|last2=Comstock|first2=Bryan|date=May 1983|title=Monerai Service Bulletin|url=https://books.google.com/books?id=nDrlpoetcl0C&pg=PA12|department=Reporting Points|magazine=]|publisher=]|volume=110|issue=5|page=12|issn=0015-4806|access-date=15 August 2016|via=]}}</ref> | |||
<!-- ==Operational history== --> | |||
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.<ref>{{cite journal|journal=Sport Aviation|title=Try a new flavor... the Monerai|date=Oct 1977|author=John Monnett}}</ref> 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.<ref name="SoaringNov83">Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 123. Soaring Society of America, November 1983. USPS 499-920</ref> | |||
<!-- ==Variants== --> | |||
The powered Monerai P and the unpowered Monerai S versions are identical structurally. | |||
<!-- ==Units using this aircraft/Operators (choose)== --> | |||
<!-- ==Development== --> | |||
<!-- ==Operational history== --> | |||
==Variants== | |||
==Specifications (variant) == | |||
;Monerai S | |||
{{aerospecs | |||
:unpowered glider | |||
|ref= | |||
;Monerai P | |||
|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show --> | |||
:] equipped with the {{convert|22|hp|kW|0|abbr=on}} ] or the {{convert|25|hp|kW|0|abbr=on}} ] engine.<ref name="SoaringNov83" /> | |||
;Monerai Max | |||
:Monerai P version with extended wing tips<ref name="SoaringNov83" /> | |||
==Aircraft on display== | |||
|crew= | |||
*]<ref name="SWSMCollection">{{cite web|url = http://swsoaringmuseum.org/collection.htm|title = Sailplanes, Hang Gliders & Motor Gliders|accessdate = 26 May 2011|last = US Southwest Soaring Museum|author-link = US Southwest Soaring Museum|authorlink = |year = 2010}}</ref> | |||
|capacity= | |||
* Serial Number 22 on display at the ], ], Windsor Locks, CT<ref>{{Cite web|url=http://neam.org/index.php?option=com_content&view=article&id=870|title = New England Air Museum}}</ref> | |||
|length m= | |||
* S/N 323, Museum of Flying, Santa Monica Airport, CA | |||
|length ft= | |||
|length in= | |||
|span m= | |||
|span ft= | |||
|span in= | |||
|swept m=<!-- swing-wings --> | |||
|swept ft=<!-- swing-wings --> | |||
|swept in=<!-- swing-wings --> | |||
|rot number=<!-- helicopters --> | |||
|rot dia m=<!-- helicopters --> | |||
|rot dia ft=<!-- helicopters --> | |||
|rot dia in=<!-- helicopters --> | |||
|dia m=<!-- airships etc --> | |||
|dia ft=<!-- airships etc --> | |||
|dia in=<!-- airships etc --> | |||
|width m=<!-- if applicable --> | |||
|width ft=<!-- if applicable --> | |||
|width in=<!-- if applicable --> | |||
|height m= | |||
|height ft= | |||
|height in= | |||
|wing area sqm= | |||
|wing area sqft= | |||
|swept area sqm=<!-- swing-wings --> | |||
|swept area sqft=<!-- swing-wings --> | |||
|rot area sqm=<!-- helicopters --> | |||
|rot area sqft=<!-- helicopters --> | |||
|volume m3=<!-- lighter-than-air --> | |||
|volume ft3=<!-- lighter-than-air --> | |||
|aspect ratio=<!-- sailplanes --> | |||
|empty weight kg= | |||
|empty weight lb= | |||
|gross weight kg= | |||
|gross weight lb= | |||
|lift kg=<!-- lighter-than-air --> | |||
|lift lb=<!-- lighter-than-air --> | |||
==Specifications (Monerai S) == | |||
|eng1 number= | |||
{{Aircraft specs | |||
|eng1 type= | |||
|prime units? = imp | |||
|eng1 kw=<!-- prop engines --> | |||
|crew=One pilot | |||
|eng1 hp=<!-- prop engines --> | |||
|length m=5.97 | |||
|eng1 kn=<!-- jet/rocket engines --> | |||
|length ft=19 | |||
|eng1 lbf=<!-- jet/rocket engines --> | |||
|length in=7 | |||
|eng1 kn-ab=<!-- afterburners --> | |||
|span m=10.97 | |||
|eng1 lbf-ab=<!-- afterburners --> | |||
|span ft=36 | |||
|eng2 number= | |||
| |
|span in=0 | ||
|height m=1.32 | |||
|eng2 kw=<!-- prop engines --> | |||
|height ft=4 | |||
|eng2 hp=<!-- prop engines --> | |||
|height in=4 | |||
|eng2 kn=<!-- jet/rocket engines --> | |||
|wing area sqm=7.25 | |||
|eng2 lbf=<!-- jet/rocket engines --> | |||
|wing area sqft=78 | |||
|eng2 kn-ab=<!-- afterburners --> | |||
|aspect ratio=16.6:1 | |||
|eng2 lbf-ab=<!-- afterburners --> | |||
|empty weight kg=100 | |||
|empty weight lb=220 | |||
|max speed kmh= | |||
|gross weight kg=204 | |||
|max speed mph= | |||
|gross weight lb=450 | |||
|max speed mach=<!-- supersonic aircraft --> | |||
| |
|max speed kmh=193 | ||
| |
|max speed mph=120 | ||
|glide ratio=<!-- sailplanes -->28:1 at 60mph | |||
|range km= | |||
|sink rate ms=<!-- sailplanes -->0.85 | |||
|range miles= | |||
|sink rate note=<!-- sailplanes -->at 55 mph: 167 | |||
|endurance h=<!-- if range unknown --> | |||
|endurance min=<!-- if range unknown --> | |||
|ceiling m= | |||
|ceiling ft= | |||
|glide ratio=<!-- sailplanes --> | |||
|climb rate ms= | |||
|climb rate ftmin= | |||
|sink rate ms=<!-- sailplanes --> | |||
|sink rate ftmin=<!-- sailplanes --> | |||
|armament1= | |||
|armament2= | |||
|armament3= | |||
|armament4= | |||
|armament5= | |||
|armament6= | |||
}} | }} | ||
<!-- ==See also== --> | <!-- ==See also== --> | ||
{{aircontent | {{aircontent | ||
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==References== | ==References== | ||
{{Reflist}} | |||
* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London |pages= }} | |||
* {{cite book |
* {{cite book |title=Jane's All the World's Aircraft 1985-86 |page=756}} | ||
* {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages= }} | |||
== External links == | |||
{{commons category|Monnett Monerai}} | |||
* | |||
{{ |
{{Monnett aircraft}} | ||
] | |||
'''Monerai gliders''' refer to three models of kit built ]s manufactures by Monerai corporation. Models available incluse: | |||
* Monerai P (]) | |||
* Monerai S (unpowered glider) | |||
* Monerai Max (Monerai P version with extended wing tips) | |||
Both the powered (Monerai P) and unpowered (Monerai S) versions are identical structurally. | |||
The Monerai is a 80's era kit built aircraft of ]/] that assembles in more or less 600 hours. It has bonded wing skins and incorporates 90 Deg Flaps for glide path control. | |||
A version with extended wing tips also available (Monerai Max) which increases the span to 12 m (39 ft). | |||
== Specifications Sheet == | |||
=== Monerai S / Monerai Max === | |||
{| class="wikitable" width="70%" | |||
! !! Monerai !! Monerai Max (Extended Tips) | |||
|- | |||
|Stall speed || 38 mph || 38 mph | |||
|- | |||
|Sink || 2.8 ft/s@55 mph || 2.2 ft/s@55 mph | |||
|- | |||
|LD || 28/1 at 60 mph || 32/1 at 60 mph | |||
|- | |||
|Vne || 120 mph || 120 mph | |||
|- | |||
|Vfe || +90°, -12° 90 mph || +90°, -12° 90 mph | |||
|- | |||
|Length || 19 ft 7 in || 19 ft 7 in | |||
|- | |||
|Height || 35 in/52 in || 35 in | |||
|- | |||
|Area || 78 ft² || 84.5 ft² | |||
|- | |||
|Span || 36 ft (11 m) || 39 ft (12 m) | |||
|- | |||
|Chord || 26 in || 26 in | |||
|- | |||
|Airfoil || FX61-192 mod || FX61-192 mod | |||
|- | |||
|Empty weight || 220 lb || 230 lb | |||
|- | |||
|Gross weight || 450 lb (+- 6 g) || 450 lb (+- 6 g) | |||
|} | |||
=== Monerai P === | |||
{| class="wikitable" width="70%" | |||
|- | |||
|Empty weight || 270 lb | |||
|- | |||
|Gross weight || 500 lb (+- 5.2 g) | |||
|- | |||
|Stall || 40 mph | |||
|- | |||
|LD || 22/1 @60 mph | |||
|- | |||
|Engine || Zenoah 250 single cylinder 2 cycle | |||
|- | |||
|Fuel capacity || 1 US gal | |||
|- | |||
|Engine duration || 30 minutes | |||
|- | |||
|Rate of climb || 400 ft/min | |||
|} | |||
== External links == | |||
* | |||
] | |||
] | ] | ||
] | |||
] | |||
] | |||
] | |||
] |
Latest revision as of 00:12, 10 September 2024
Monerai | |
---|---|
Monerai S | |
General information | |
Type | Sailplane |
National origin | United States |
Manufacturer | Monnett Experimental Aircraft |
Designer | John Monnett |
Number built | 100 by January 1984 from 375 kits sold |
History | |
Introduction date | 1978 |
First flight | 1978 |
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.
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
- US Southwest Soaring Museum
- Serial Number 22 on display at the New England Air Museum, Bradley International Airport, Windsor Locks, CT
- S/N 323, Museum of Flying, Santa Monica Airport, CA
Specifications (Monerai S)
General characteristics
- Crew: One pilot
- Length: 19 ft 7 in (5.97 m)
- Wingspan: 36 ft 0 in (10.97 m)
- Height: 4 ft 4 in (1.32 m)
- Wing area: 78 sq ft (7.25 m)
- Aspect ratio: 16.6:1
- Empty weight: 220 lb (100 kg)
- Gross weight: 450 lb (204 kg)
Performance
- Maximum speed: 120 mph (193 km/h, 100 kn)
- Maximum glide ratio: 28:1 at 60mph
- Rate of sink: 167 ft/min (0.85 m/s) at 55 mph: 167
References
- 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.
- John Monnett (Oct 1977). "Try a new flavor... the Monerai". Sport Aviation.
- ^ Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 123. Soaring Society of America, November 1983. USPS 499-920
- US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.
- "New England Air Museum".
- Jane's All the World's Aircraft 1985-86. p. 756.
External links
Aircraft designed by John Monnett | |
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Aircraft |