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词条 Paraavis Vityaz
释义

  1. Design and development

  2. Specifications (Vityaz)

  3. References

  4. External links

name=Vityaz image= caption=

}}{{Infobox Aircraft Type

type=Paramotor national origin=Russia manufacturer=Paraavis designer= first flight= introduced= retired= status= In production (2015) primary user= more users= produced= early 2000s - present number built= program cost= unit cost= US$3,200 (2004) developed from= variants with their own articles=
}}

The Paraavis Vityaz (Russian: "Витязь", English: "Knight") is a Russia paramotor, designed and produced by Paraavis of Moscow for powered paragliding. The aircraft is supplied complete and ready-to-fly.[1]

Design and development

The Vityaz was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place or two-place accommodation and a single engine in pusher configuration. Early versions were powered by a Zanzottera MZ 34 {{convert|27.5|hp|kW|0|abbr=on}} motor with a 2.5:1 ratio reduction drive and a {{convert|125|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. Later versions feature a Simonini Mini 2 Plus of {{convert|28|hp|kW|0|abbr=on}} or a Simonini Mini 2 Evo of {{convert|33|hp|kW|0|abbr=on}} and a two-bladed wooden propeller. The fuel tank capacity is {{convert|8|l}}, while later versions offer an option of {{convert|15|l}}. The aircraft is built in two versions, one predominantly from aluminium and the other from titanium.[1][2]

As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]

Specifications (Vityaz)

{{Aircraft specs
|ref=Bertrand[1]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
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|airfoil=
|empty weight kg=31
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|8|l}}
|more general=


|eng1 number=1
|eng1 name=Zanzottera MZ 34
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a 2.5:1 reduction drive
|eng1 kw=
|eng1 hp=27.5
|prop blade number=2
|prop name=wooden, fixed pitch
|prop dia m=1.25
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
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|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|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=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|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=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 71. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
2. ^{{cite web|url=http://www.paraavis.com/en/paramotors/185-vityaz.html|title=Vityaz|work=paraavis.com|accessdate=10 November 2015}}

External links

  • {{Official website|http://www.paraavis.com/en/paramotors/185-vityaz.html}}
{{Paraavis aircraft}}

4 : Paraavis aircraft|Russian ultralight aircraft 2000–2009|Single-engined pusher aircraft|Paramotors

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