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词条 Let-Mont Tulak
释义

  1. Design and development

  2. Operational history

  3. Specifications (Tulak)

  4. References

  5. External links

name= Tulak image=Let-Mont TUL-01 Tulak Piper UL AN1625466.jpg caption=

}}{{Infobox Aircraft Type

type=Microlight aircraft national origin=Czech Republic manufacturer=Let-Mont sro designer= first flight= introduced= retired= status= Production completed primary user= more users= produced= number built=10 (1998) program cost= unit cost= €31,500 (2011) developed from= variants with their own articles=
}}

The Let-Mont Tulak ({{lang-en|rogue, wanderer or tramp}}) is a Czech microlight aircraft that was designed and produced by Let-Mont sro of Vikýřovice. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft or a kit for amateur construction.[1][2]

The aircraft was marketed in Austria and Germany under the name Amigo.[2]

Design and development

The aircraft was designed to comply with the European Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}. It was also marketed in the United States as a kit only for the US homebuilt category.[1][2]

The Tulak features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.[1][2]

The aircraft fuselage is made from welded steel tubing, with the whole aircraft covered in doped aircraft fabric. Its {{convert|10.0|m|ft|1|abbr=on}} span wing employs a Clark Y airfoil, mounts flaps, has a wing area of {{convert|13.01|m2|sqft|abbr=on}} and is supported by "V" struts and jury struts. The standard engine used is the {{convert|50|hp|kW|0|abbr=on}} Rotax 503 two-stroke and {{convert|80|hp|kW|0|abbr=on}} Rotax 912 four-stroke powerplant, although a four-stroke BMW boxer engine was also available as a factory option[1][2][3]

The Tulak has a typical empty weight of {{convert|230|kg|lb|abbr=on}} and a gross weight of {{convert|450|kg|lb|abbr=on}}, giving a useful load of {{convert|220|kg|lb|abbr=on}}.[1]

The manufacturer estimated the construction time from the supplied kit as 700 hours.[1]

Operational history

By 1998 the company reported that 10 aircraft were completed and flying.[1]

In September 2014 no examples were registered in the United States with the Federal Aviation Administration.[4]

Specifications (Tulak)

{{Aircraft specs
|ref=AeroCrafter and The Incomplete Guide to Airfoil Usage[1][3]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=31.50
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=140.0
|wing area note=
|aspect ratio=
|airfoil=Clark Y
|empty weight kg=
|empty weight lb=507
|empty weight note=
|gross weight kg=
|gross weight lb=992
|gross weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Rotax 503
|eng1 type=twin cylinder, air-cooled, two stroke aircraft engine
|eng1 kw=
|eng1 hp=50
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=93
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=68
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=27
|stall speed kts=
|stall speed note=flaps down
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=+6/-6
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=550
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=7.1
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 195. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}
2. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 146. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
3. ^{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 2 January 2014|last = Lednicer |first = David |year = 2010}}
4. ^{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=TULAK&PageNo=1|title = Make / Model Inquiry Results|accessdate = 11 September 2014|last = Federal Aviation Administration|date = 11 September 2014}}

External links

{{Commons category|Let-Mont Tulak}}{{Let-Mont aircraft}}

7 : Let-Mont aircraft|Czech and Czechoslovakian sport aircraft 1990–1999|Czech and Czechoslovakian ultralight aircraft 1990–1999|Czech and Czechoslovakian civil utility aircraft 1990–1999|Single-engined tractor aircraft|High-wing aircraft|Homebuilt aircraft

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